[go: up one dir, main page]

GB2455310B - A combustion apparatus for a gas turbine engine - Google Patents

A combustion apparatus for a gas turbine engine

Info

Publication number
GB2455310B
GB2455310B GB0723701A GB0723701A GB2455310B GB 2455310 B GB2455310 B GB 2455310B GB 0723701 A GB0723701 A GB 0723701A GB 0723701 A GB0723701 A GB 0723701A GB 2455310 B GB2455310 B GB 2455310B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
combustion apparatus
combustion
engine
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 - Fee Related
Application number
GB0723701A
Other versions
GB0723701D0 (en
GB2455310A (en
Inventor
Nigel Anthony Wilbraham
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.)
Siemens AG
Siemens Corp
Original Assignee
Siemens AG
Siemens Corp
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 Siemens AG, Siemens Corp filed Critical Siemens AG
Priority to GB0723701A priority Critical patent/GB2455310B/en
Publication of GB0723701D0 publication Critical patent/GB0723701D0/en
Publication of GB2455310A publication Critical patent/GB2455310A/en
Application granted granted Critical
Publication of GB2455310B publication Critical patent/GB2455310B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling combustion
    • F23N5/26—Details
    • 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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • F23R3/26—Controlling the air flow
    • 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
    • F23R3/34—Feeding into different combustion zones
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2241/00—Applications
    • F23N2241/20—Gas turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
GB0723701A 2007-12-04 2007-12-04 A combustion apparatus for a gas turbine engine Expired - Fee Related GB2455310B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0723701A GB2455310B (en) 2007-12-04 2007-12-04 A combustion apparatus for a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0723701A GB2455310B (en) 2007-12-04 2007-12-04 A combustion apparatus for a gas turbine engine

Publications (3)

Publication Number Publication Date
GB0723701D0 GB0723701D0 (en) 2008-01-16
GB2455310A GB2455310A (en) 2009-06-10
GB2455310B true GB2455310B (en) 2009-11-18

Family

ID=38982954

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0723701A Expired - Fee Related GB2455310B (en) 2007-12-04 2007-12-04 A combustion apparatus for a gas turbine engine

Country Status (1)

Country Link
GB (1) GB2455310B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102519056A (en) * 2011-12-26 2012-06-27 南京航空航天大学 Small-size precombustion chamber for engine

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5417070A (en) * 1992-11-24 1995-05-23 Rolls-Royce Plc Fuel injection apparatus
US5941075A (en) * 1996-09-05 1999-08-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Fuel injection system with improved air/fuel homogenization
EP1201995A2 (en) * 2000-10-23 2002-05-02 ALSTOM Power N.V. Gas turbine engine combustion system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5417070A (en) * 1992-11-24 1995-05-23 Rolls-Royce Plc Fuel injection apparatus
US5941075A (en) * 1996-09-05 1999-08-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Fuel injection system with improved air/fuel homogenization
EP1201995A2 (en) * 2000-10-23 2002-05-02 ALSTOM Power N.V. Gas turbine engine combustion system

Also Published As

Publication number Publication date
GB0723701D0 (en) 2008-01-16
GB2455310A (en) 2009-06-10

Similar Documents

Publication Publication Date Title
GB2438696B (en) A gas turbine engine
GB2450139B (en) An aerofoil for a gas turbine engine
EP2153051A4 (en) A masking arrangement for a gas turbine engine
GB0608859D0 (en) A gas turbine engine
GB0610800D0 (en) Combustion chamber for a gas turbine engine
GB0809336D0 (en) A gas turbine engine arrangement
GB2436128B (en) Gas turbine engine
PL2145080T3 (en) Gas turbine engine for helicoptere comprising a gas generator and a free turbine
GB2443194B (en) Gas turbine engine
GB0707170D0 (en) Method and apparatus for operating a gas turbine engine
GB0601220D0 (en) Aerofoils for gas turbine engines
GB0603285D0 (en) A gas turbine engine
EP2084455A4 (en) Combustion apparatus for a gas boiler
GB0822676D0 (en) A gas turbine engine
PL2331878T3 (en) Combustor assembly for a gas turbine engine
EP2519729A4 (en) Exhaust for a gas turbine engine
PL1980740T3 (en) Engine gas fuel supply apparatus
GB0912166D0 (en) A turbofan gas turbine engine
GB2461778B (en) A centering device for a gas turbine engine.
GB0617252D0 (en) Wall elements for gas turbine engine components
GB2445952B (en) A gas turbine engine
EP2148065A4 (en) Gas turbine engine
GB2434837B (en) A containment system for a gas turbine engine
GB0624294D0 (en) A transition duct for a gas turbine engine
EP2235345A4 (en) A gas turbine engine

Legal Events

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

Effective date: 20111204