GB904460A - Gas turbine engine combustion chamber - Google Patents

Gas turbine engine combustion chamber

Info

Publication number
GB904460A
GB904460A GB1448560A GB1448560A GB904460A GB 904460 A GB904460 A GB 904460A GB 1448560 A GB1448560 A GB 1448560A GB 1448560 A GB1448560 A GB 1448560A GB 904460 A GB904460 A GB 904460A
Authority
GB
United Kingdom
Prior art keywords
annular
flame
combustion chamber
flame tubes
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
GB1448560A
Inventor
Arthur Henry Lefebvre
Herbert Frank Smith
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 GB1448560A priority Critical patent/GB904460A/en
Publication of GB904460A publication Critical patent/GB904460A/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

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)

Abstract

904,460. Generating combustion products under pressure. ROLLS-ROYCE Ltd. April 18, 1961 [April 25, 1960], No. 14485/60. Class 51 (1). An annular combustion chamber comprises two concentric annular flame tubes between which is an annular duct supplying all the primary air to the flame tubes through the adjacent walls of the flame tubes and annular duct. In Fig. 2, the annular flame tubes 23, 24 surround an annular air duct 22. Fuel injectors 26 are fitted to each flame tube, the flame tube 24 being fitted with ignition means 29 and at least one interconnector 35 is provided. Primary air is admitted to the flame tubes by apertures 31 and dilution air by ducts 33, 34. Baffles 30 deflect a minor proportion of the inlet air into spaces 27, 28 between the flame tubes and the combustion chamber casings 10-20 for cooling. Specification 874,644 is referred to.
GB1448560A 1960-04-25 1960-04-25 Gas turbine engine combustion chamber Expired GB904460A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1448560A GB904460A (en) 1960-04-25 1960-04-25 Gas turbine engine combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1448560A GB904460A (en) 1960-04-25 1960-04-25 Gas turbine engine combustion chamber

Publications (1)

Publication Number Publication Date
GB904460A true GB904460A (en) 1962-08-29

Family

ID=10042050

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1448560A Expired GB904460A (en) 1960-04-25 1960-04-25 Gas turbine engine combustion chamber

Country Status (1)

Country Link
GB (1) GB904460A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2504654A1 (en) * 1981-04-22 1982-10-29 Gen Electric ADVANCED COMBUSTION CHAMBER
DE102011089242A1 (en) * 2011-12-20 2013-06-20 Siemens Aktiengesellschaft Combustion system for gas turbine, has two annular combustion chambers, which are arranged parallel to each other relative to flow direction of combustion gas in coaxial manner

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2504654A1 (en) * 1981-04-22 1982-10-29 Gen Electric ADVANCED COMBUSTION CHAMBER
DE102011089242A1 (en) * 2011-12-20 2013-06-20 Siemens Aktiengesellschaft Combustion system for gas turbine, has two annular combustion chambers, which are arranged parallel to each other relative to flow direction of combustion gas in coaxial manner

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