GB2009860A - Gas turbine combustion chambers - Google Patents

Gas turbine combustion chambers

Info

Publication number
GB2009860A
GB2009860A GB7847778A GB7847778A GB2009860A GB 2009860 A GB2009860 A GB 2009860A GB 7847778 A GB7847778 A GB 7847778A GB 7847778 A GB7847778 A GB 7847778A GB 2009860 A GB2009860 A GB 2009860A
Authority
GB
United Kingdom
Prior art keywords
inlet
gas turbine
combustion chambers
turbine combustion
fuel
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.)
Granted
Application number
GB7847778A
Other versions
GB2009860B (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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB7847778A priority Critical patent/GB2009860B/en
Publication of GB2009860A publication Critical patent/GB2009860A/en
Application granted granted Critical
Publication of GB2009860B publication Critical patent/GB2009860B/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

The combustion chamber has at least one primary air inlet 13 having means 15 defining an entry to the inlet and a fuel supply system including at least one orifice 17 positioned adjacent the inlet to supply, in use, a film of fuel over the means 15. Fuel is thus drawn into the combustion chamber entrained in the vortex system which is set up at the inlet. The fuel supply pipe 16 may extend along the wall 11 as shown, extend radially to the means 15, or be positioned inside the wall 11. <IMAGE>
GB7847778A 1977-12-14 1978-12-08 Combustion apparatus Expired GB2009860B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7847778A GB2009860B (en) 1977-12-14 1978-12-08 Combustion apparatus

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB5207677 1977-12-14
GB7847778A GB2009860B (en) 1977-12-14 1978-12-08 Combustion apparatus

Publications (2)

Publication Number Publication Date
GB2009860A true GB2009860A (en) 1979-06-20
GB2009860B GB2009860B (en) 1982-03-03

Family

ID=26266989

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7847778A Expired GB2009860B (en) 1977-12-14 1978-12-08 Combustion apparatus

Country Status (1)

Country Link
GB (1) GB2009860B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0349635A1 (en) * 1987-12-28 1990-01-10 Sundstrand Corp Turbine combustor with tangential fuel injection and bender jets.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0349635A1 (en) * 1987-12-28 1990-01-10 Sundstrand Corp Turbine combustor with tangential fuel injection and bender jets.
EP0349635A4 (en) * 1987-12-28 1990-05-14 Sundstrand Corp Turbine combustor with tangential fuel injection and bender jets.

Also Published As

Publication number Publication date
GB2009860B (en) 1982-03-03

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Legal Events

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

Effective date: 19931208