GB639617A - Improvements in and relating to combustion chambers - Google Patents

Improvements in and relating to combustion chambers

Info

Publication number
GB639617A
GB639617A GB31441/47A GB3144147A GB639617A GB 639617 A GB639617 A GB 639617A GB 31441/47 A GB31441/47 A GB 31441/47A GB 3144147 A GB3144147 A GB 3144147A GB 639617 A GB639617 A GB 639617A
Authority
GB
United Kingdom
Prior art keywords
liner
air
dome
direct
outer housing
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
GB31441/47A
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.)
British Thomson Houston Co Ltd
Original Assignee
British Thomson Houston Co 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 British Thomson Houston Co Ltd filed Critical British Thomson Houston Co Ltd
Publication of GB639617A publication Critical patent/GB639617A/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
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Gasket Seals (AREA)

Abstract

639,617. Generating combustion products under pressure. BRITISH THOMSON-HOUSTON CO., Ltd. Nov. 27, 1947, No. 31441. Convention date, Feb. 1, 1946. [Class 51 (i)] [Also in Groups XXVI and XXVIII] A combustion chamber particularly for a gas turbine plant has a liner 7 with one end closed by a hemispherical dome 10 having a central opening 60 to receive the fuel nozzle 32 and openings 40 arranged to direct a thin sheet of air 49 over the inner surface of the dome towards the central opening. The liner is surrounded by an outer housing 11 coupled to an air adapter pipe 2. The dome is supported by brackets 34a from the adaptorpipe and has circumferentially-spaced projections 42 engaging the inner surface of the liner so as to form arcuate slots which direct a thin layer of air axially along the inner surface of the liner. An expansion joint 18 is provided between the end of the outer housing 11 and the adjacent enlarged end of the air adapter pipe. Specification 590,422, [Group XXVI], is referred to.
GB31441/47A 1946-02-01 1947-11-27 Improvements in and relating to combustion chambers Expired GB639617A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US644888A US2581999A (en) 1946-02-01 1946-02-01 Hemispherical combustion chamber end dome having cooling air deflecting means

Publications (1)

Publication Number Publication Date
GB639617A true GB639617A (en) 1950-07-05

Family

ID=24586749

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31441/47A Expired GB639617A (en) 1946-02-01 1947-11-27 Improvements in and relating to combustion chambers

Country Status (2)

Country Link
US (1) US2581999A (en)
GB (1) GB639617A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108626750A (en) * 2018-05-09 2018-10-09 中国航发湖南动力机械研究所 The burner inner liner of active control circulation area

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL74196C (en) * 1947-08-11
US2711631A (en) * 1949-06-21 1955-06-28 Hartford Nat Bank & Trust Co Gas turbine power plant
US2645081A (en) * 1949-08-19 1953-07-14 A V Roe Canada Ltd Spacing means for the wall sections of flame tubes
US2635423A (en) * 1950-08-28 1953-04-21 Edward J Oakes Igniter for internal-combustion engines
US2692478A (en) * 1951-02-24 1954-10-26 Boeing Co Turbine burner incorporating removable burner liner
US2729062A (en) * 1951-07-06 1956-01-03 Dresser Operations Inc Power plant combustion chamber
US2807934A (en) * 1951-12-06 1957-10-01 A V Roe Canada Ltd Flame tube support for a gas turbine combustion system
US2775293A (en) * 1952-09-16 1956-12-25 Hupp Corp Liquid fuel fired heating apparatus for use, especially on automotive conveyances
US2949736A (en) * 1952-10-03 1960-08-23 Rolls Royce Expansion joint with fuel drainage collector for ducting of gas turbine power plants
US2930192A (en) * 1953-12-07 1960-03-29 Gen Electric Reverse vortex combustion chamber
DE1021646B (en) * 1953-12-07 1957-12-27 Gen Elek C Company Combustion chamber
US2907171A (en) * 1954-02-15 1959-10-06 Lysholm Alf Combustion chamber inlet for thermal power plants
US2944399A (en) * 1956-05-31 1960-07-12 Gen Electric Afterburner combustion means
US3631674A (en) * 1970-01-19 1972-01-04 Gen Electric Folded flow combustion chamber for a gas turbine engine
US3916619A (en) * 1972-10-30 1975-11-04 Hitachi Ltd Burning method for gas turbine combustor and a construction thereof
US3826088A (en) * 1973-02-01 1974-07-30 Gen Electric Gas turbine engine augmenter cooling liner stabilizers and supports
US4180972A (en) * 1978-06-08 1980-01-01 General Motors Corporation Combustor support structure
US4686823A (en) * 1986-04-28 1987-08-18 United Technologies Corporation Sliding joint for an annular combustor
US4930306A (en) * 1988-05-26 1990-06-05 Sundstrand Corporation Reducing carbon buildup in a turbine engine
US5165226A (en) * 1991-08-09 1992-11-24 Pratt & Whitney Canada, Inc. Single vortex combustor arrangement
US5329772A (en) * 1992-12-09 1994-07-19 General Electric Company Cast slot-cooled single nozzle combustion liner cap
KR0162337B1 (en) * 1995-04-03 1999-03-20 구자홍 Oil supply apparatus of a hermetic compressor
US8769963B2 (en) * 2007-01-30 2014-07-08 Siemens Energy, Inc. Low leakage spring clip/ring combinations for gas turbine engine
US8438854B2 (en) * 2008-05-23 2013-05-14 Honeywell International Inc. Pre-diffuser for centrifugal compressor

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432359A (en) * 1947-12-09 Internal-combustion turbine power
FR337447A (en) * 1903-12-05 1904-04-09 Gaston Charles Emile De Bonnec Generator for continuous combustion engines
US996324A (en) * 1905-04-17 1911-06-27 Sebastian Ziani De Ferranti Propulsion apparatus for ships, boats, and the like.
DE376570C (en) * 1921-06-14 1923-05-30 Hans Pfeil Oil or gas firing
US1828326A (en) * 1929-08-10 1931-10-20 Lanser Alfred Burner
US1960810A (en) * 1930-07-26 1934-05-29 Doherty Res Co Gas turbine
US2107365A (en) * 1934-04-21 1938-02-08 United Shoe Machinery Corp Heating apparatus suitable for use in shoemaking
US2229805A (en) * 1938-10-24 1941-01-28 Lester S Graves Combustion apparatus for producing fluid under pressure
US2268464A (en) * 1939-09-29 1941-12-30 Bbc Brown Boveri & Cie Combustion chamber
NL82403C (en) * 1939-12-09
US2361871A (en) * 1942-06-20 1944-10-31 Roberts William Air and fuel preheating oil burner
US2465525A (en) * 1943-12-15 1949-03-29 Daniel And Florence Guggenheim Reaction combustion chamber for unconfined charges or detonative fuel fed intermittently to the combustion chamber
BE461591A (en) * 1944-03-16
GB585763A (en) * 1944-11-01 1947-02-24 Armstrong Siddeley Motors Ltd Improvements relating to combustion chambers

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108626750A (en) * 2018-05-09 2018-10-09 中国航发湖南动力机械研究所 The burner inner liner of active control circulation area

Also Published As

Publication number Publication date
US2581999A (en) 1952-01-08

Similar Documents

Publication Publication Date Title
GB639617A (en) Improvements in and relating to combustion chambers
GB682128A (en) Gas turbine nozzle boxes
GB584820A (en) Improvements relating to internal combustion prime movers
GB554112A (en) Method and device for cooling combustion chambers, particularly for gas turbines or the like
GB650462A (en) Improvements in or relating to combustion apparatus
GB1055234A (en) Ultra-high temperature combustion chambers
GB616695A (en) Improvements in and relating to gas turbine power plants
GB693846A (en) Vaporizer-type combustion apparatus for gas turbine engines
GB587083A (en) Improvements in combustion chambers for internal combustion turbines
GB627644A (en) Improvements relating to gas-turbine-engines and combustion-equipment therefor
GB699267A (en) Improvements in or relating to combustion turbine units
GB648699A (en) Improvements in or relating to gas-turbine engine fuel systems and liquid fuel injectors therefor
GB565952A (en) Improvements in means for generating a mixture of steam and combustion products under pressure
GB585763A (en) Improvements relating to combustion chambers
GB620270A (en) Improvements in or relating to turbine apparatus
GB697027A (en) Combustion chambers for prime movers
GB710589A (en) Combustion chambers for jet engines or gas turbines
GB682778A (en) Improvements relating to combustion chambers for prime movers
GB576545A (en) Improvements relating to combustion chambers for prime movers
GB700705A (en) Combustion chambers for jet propulsion engines, gas turbines or other prime movers
GB597853A (en) Improvement in combustion chambers for internal combustion gas turbines with heat exchangers
GB672530A (en) Improvements in gas turbine combustion chambers
GB627962A (en) A combustion chamber for an internal-combustion turbine plant
GB621065A (en) Improvements in compressors
GB729163A (en) Improvements in or relating to cyclone furnaces