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GB697027A - Combustion chambers for prime movers - Google Patents

Combustion chambers for prime movers

Info

Publication number
GB697027A
GB697027A GB28917/50A GB2891750A GB697027A GB 697027 A GB697027 A GB 697027A GB 28917/50 A GB28917/50 A GB 28917/50A GB 2891750 A GB2891750 A GB 2891750A GB 697027 A GB697027 A GB 697027A
Authority
GB
United Kingdom
Prior art keywords
air
tube
holes
end wall
flame tube
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
GB28917/50A
Inventor
John Stanley Clarke
William Edmund Gregory
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.)
ZF International UK Ltd
Original Assignee
Joseph Lucas 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 Joseph Lucas Ltd filed Critical Joseph Lucas Ltd
Priority to GB28917/50A priority Critical patent/GB697027A/en
Priority to FR1045490D priority patent/FR1045490A/en
Publication of GB697027A publication Critical patent/GB697027A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • 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
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

697,027. Generating combustion products under pressure. LUCAS. Ltd., J. Nov. 16, 1951 [Nov. 27, 1950], No. 28917/50. Class 51(i) In an air jacketed type of combustion chamber for a gas turbine or jet propulsion engine, the inlet end of the flame tube has an annular sheet metal partition, the outer surface a of which constitutes the inner wall of the air supply passage b to the surrounding air jacket c, and the inner surface of which forms a cylindrical duct d leading to an air swirling means g through which air passes to the axial region of the flame tube. The end wall e of the flame tube has a circumferential flange p which meets the inner surface of the annular portion a. The end wall e is formed of overlapping plates which have holes n through which air can pass to cool the end wall, air being admitted to the annular partition through holes o in the outer surface or in the cylindrical duct d. A tube h is disposed within the duct part d and the fuel nozzle j is disposed within the tube, air passing through holes m to effect a scouring action on the nozzle.
GB28917/50A 1950-11-27 1950-11-27 Combustion chambers for prime movers Expired GB697027A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB28917/50A GB697027A (en) 1950-11-27 1950-11-27 Combustion chambers for prime movers
FR1045490D FR1045490A (en) 1950-11-27 1951-11-26 Combustion chamber for engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB28917/50A GB697027A (en) 1950-11-27 1950-11-27 Combustion chambers for prime movers

Publications (1)

Publication Number Publication Date
GB697027A true GB697027A (en) 1953-09-16

Family

ID=10283278

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28917/50A Expired GB697027A (en) 1950-11-27 1950-11-27 Combustion chambers for prime movers

Country Status (2)

Country Link
FR (1) FR1045490A (en)
GB (1) GB697027A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2973624A (en) * 1955-10-26 1961-03-07 Gen Electric Cowled dome liners
US2994196A (en) * 1954-03-02 1961-08-01 Bristol Aero Engines Ltd Flame tubes for use in combustion systems of gas turbine engines
US3057158A (en) * 1959-01-29 1962-10-09 Rolls Royce Temperature responsive throttle for combustion chamber cooling air
US3430443A (en) * 1966-02-21 1969-03-04 Bristol Siddeley Engines Ltd Liquid fuel combusion apparatus for gas turbine engines
US3854285A (en) * 1973-02-26 1974-12-17 Gen Electric Combustor dome assembly
EP0584906A2 (en) * 1992-06-12 1994-03-02 General Electric Company Film cooling starter geometry for combustor liners

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2994196A (en) * 1954-03-02 1961-08-01 Bristol Aero Engines Ltd Flame tubes for use in combustion systems of gas turbine engines
US2973624A (en) * 1955-10-26 1961-03-07 Gen Electric Cowled dome liners
US3057158A (en) * 1959-01-29 1962-10-09 Rolls Royce Temperature responsive throttle for combustion chamber cooling air
US3430443A (en) * 1966-02-21 1969-03-04 Bristol Siddeley Engines Ltd Liquid fuel combusion apparatus for gas turbine engines
US3854285A (en) * 1973-02-26 1974-12-17 Gen Electric Combustor dome assembly
EP0584906A2 (en) * 1992-06-12 1994-03-02 General Electric Company Film cooling starter geometry for combustor liners
EP0584906A3 (en) * 1992-06-12 1994-05-04 General Electric Company Film cooling starter geometry for combustor liners
US5479772A (en) * 1992-06-12 1996-01-02 General Electric Company Film cooling starter geometry for combustor liners

Also Published As

Publication number Publication date
FR1045490A (en) 1953-11-26

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