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GB2073396B - Gas turbine combustion chambers - Google Patents

Gas turbine combustion chambers

Info

Publication number
GB2073396B
GB2073396B GB8010674A GB8010674A GB2073396B GB 2073396 B GB2073396 B GB 2073396B GB 8010674 A GB8010674 A GB 8010674A GB 8010674 A GB8010674 A GB 8010674A GB 2073396 B GB2073396 B GB 2073396B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
combustion chambers
turbine combustion
chambers
gas
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
GB8010674A
Other versions
GB2073396A (en
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 GB8010674A priority Critical patent/GB2073396B/en
Publication of GB2073396A publication Critical patent/GB2073396A/en
Application granted granted Critical
Publication of GB2073396B publication Critical patent/GB2073396B/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
    • F23R3/06—Arrangement of apertures along the flame tube

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB8010674A 1980-03-29 1980-03-29 Gas turbine combustion chambers Expired GB2073396B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8010674A GB2073396B (en) 1980-03-29 1980-03-29 Gas turbine combustion chambers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8010674A GB2073396B (en) 1980-03-29 1980-03-29 Gas turbine combustion chambers

Publications (2)

Publication Number Publication Date
GB2073396A GB2073396A (en) 1981-10-14
GB2073396B true GB2073396B (en) 1984-02-22

Family

ID=10512495

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8010674A Expired GB2073396B (en) 1980-03-29 1980-03-29 Gas turbine combustion chambers

Country Status (1)

Country Link
GB (1) GB2073396B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6286317B1 (en) * 1998-12-18 2001-09-11 General Electric Company Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity
US6260359B1 (en) * 1999-11-01 2001-07-17 General Electric Company Offset dilution combustor liner
FR2856468B1 (en) 2003-06-17 2007-11-23 Snecma Moteurs TURBOMACHINE ANNULAR COMBUSTION CHAMBER
US20140216044A1 (en) * 2012-12-17 2014-08-07 United Technologoes Corporation Gas turbine engine combustor heat shield with increased film cooling effectiveness

Also Published As

Publication number Publication date
GB2073396A (en) 1981-10-14

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee