GB1036677A - Combustion equipment for a gas turbine engine - Google Patents

Combustion equipment for a gas turbine engine

Info

Publication number
GB1036677A
GB1036677A GB2083265A GB2083265A GB1036677A GB 1036677 A GB1036677 A GB 1036677A GB 2083265 A GB2083265 A GB 2083265A GB 2083265 A GB2083265 A GB 2083265A GB 1036677 A GB1036677 A GB 1036677A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
flame tube
pipe
combustion equipment
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
GB2083265A
Inventor
Stewart Crichton Miller
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB2083265A priority Critical patent/GB1036677A/en
Priority to DE19661476880 priority patent/DE1476880A1/en
Publication of GB1036677A publication Critical patent/GB1036677A/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
    • F23R3/045—Air inlet arrangements using pipes

Abstract

1,036,677. Gas turbine combustion chambers. ROLLS-ROYCE Ltd. May 17, 1965, No. 20832/65. Heading F1L. A gas turbine engine cylindrical flame tube 16 has a series of short pipes 26 directing air radially inwards towards a combustion zone 25. Each pipe 26 is welded by a flange 31 at its upstream side to the flame tube wall 22 and is spaced from the wall at its downstream side to form a gap 32 through which air 33 flows to cool the periphery of the pipe. Each pipe extends radially further into the flame tube at its downstream side than at its upstream side.
GB2083265A 1965-05-17 1965-05-17 Combustion equipment for a gas turbine engine Expired GB1036677A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB2083265A GB1036677A (en) 1965-05-17 1965-05-17 Combustion equipment for a gas turbine engine
DE19661476880 DE1476880A1 (en) 1965-05-17 1966-05-16 Combustion device for gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2083265A GB1036677A (en) 1965-05-17 1965-05-17 Combustion equipment for a gas turbine engine

Publications (1)

Publication Number Publication Date
GB1036677A true GB1036677A (en) 1966-07-20

Family

ID=10152455

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2083265A Expired GB1036677A (en) 1965-05-17 1965-05-17 Combustion equipment for a gas turbine engine

Country Status (2)

Country Link
DE (1) DE1476880A1 (en)
GB (1) GB1036677A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2018641C2 (en) * 1970-04-18 1972-05-10 Motoren Turbinen Union REVERSE COMBUSTION CHAMBER FOR GAS TURBINE ENGINES

Also Published As

Publication number Publication date
DE1476880B2 (en) 1970-11-12
DE1476880A1 (en) 1969-10-23

Similar Documents

Publication Publication Date Title
GB790293A (en) Improvements in or relating to heat-resisting wall structures for gas-turbine enginecombustion equipment
GB610641A (en) Improvements in or relating to combustion plants with gas-cooled combustion chambers
GB1108705A (en) Improvements in cooling structure or combustion chamber
GB1010338A (en) Means for supporting the downstream end of a combustion chamber in a gas turbine engine
GB1179166A (en) An Annular Combustion Chamber for a Gas Turbine Engine.
GB1138547A (en) Improvements in cooling structure
GB1037955A (en) Cooling arrangement for crossover tubes, linking flame tubes in a combustion chamber
GB1040390A (en) Gas turbine engine
GB1037923A (en) Combustion chamber for a gas turbine
GB1344359A (en) Combustion equipment for gas turbine engines
GB970189A (en) Combustion equipment for a gas turbine engine
GB1089467A (en) Improvements in or relating to gas turbines
GB1035541A (en) Combustion equipment for a gas turbine engine
GB762596A (en) A combustion chamber, particularly for a gas turbine engine
GB721209A (en) Combustion apparatus
GB669751A (en) Improvements relating to combustion chambers for gas turbine plants and the like
GB1036677A (en) Combustion equipment for a gas turbine engine
GB1435820A (en) Gas turbine combustion apparatus liner
GB1442350A (en) Gas turbine engine combustion equipment
GB845971A (en) Improvements relating to combustion chambers for gas turbine engines
GB887639A (en) Combustion equipment for a gas turbine engine
GB1060095A (en) Improvements relating to the flow of a cooling fluid
GB965152A (en) Improvements in or relating to primary air control devices for gas-turbine engine combustion chambers
GB543918A (en) Improvements and relating to combustion chambers
GB1150344A (en) Combustion Apparatus for Gas Turbine Engines