GB0224080D0 - Fuel injection system for a gas turbine - Google Patents

Fuel injection system for a gas turbine

Info

Publication number: GB0224080D0
Authority: GB; United Kingdom
Prior art keywords: fuel injection; gas turbine; injection system; turbine; fuel
Prior art date: 2000-04-28
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

GBGB0224080.2A

Other versions

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.)

TURBEC AB

Original Assignee

TURBEC AB

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.)

2000-04-28

Filing date

2001-04-27

Publication date

2002-11-27

2001-04-27 Application filed by TURBEC AB filed Critical TURBEC AB

2002-11-27 Publication of GB0224080D0 publication Critical patent/GB0224080D0/en

2002-12-24 Publication of GB2376721A publication Critical patent/GB2376721A/en

2004-07-07 Application granted granted Critical

2004-07-07 Publication of GB2376721B publication Critical patent/GB2376721B/en

2021-04-27 Anticipated expiration legal-status Critical

Status Expired - Fee Related legal-status Critical Current

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/263—Control of fuel supply by means of fuel metering valves

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Feeding And Controlling Fuel (AREA)
Fluidized-Bed Combustion And Resonant Combustion (AREA)
Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

GB0224080A 2000-04-28 2001-04-27 Fuel injection system for a gas turbine Expired - Fee Related GB2376721B (en)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
SE0001552A SE522267C2 (en)	2000-04-28	2000-04-28	Fuel injection for a gas turbine
PCT/SE2001/000931 WO2001083965A1 (en)	2000-04-28	2001-04-27	Fuel injection system for a gas turbine

Publications (3)

Publication Number	Publication Date
GB0224080D0 true GB0224080D0 (en)	2002-11-27
GB2376721A GB2376721A (en)	2002-12-24
GB2376721B GB2376721B (en)	2004-07-07

Family

ID=20279462

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
GB0224080A Expired - Fee Related GB2376721B (en)	2000-04-28	2001-04-27	Fuel injection system for a gas turbine

Country Status (5)

Country	Link
AU (1)	AU2001252845A1 (en)
DE (1)	DE10196104B8 (en)
GB (1)	GB2376721B (en)
SE (1)	SE522267C2 (en)
WO (1)	WO2001083965A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
SE521293C2 (en)	2001-02-06	2003-10-21	Volvo Aero Corp	Method and apparatus for supplying fuel to a combustion chamber
ITMI20111576A1 (en)	2011-09-02	2013-03-03	Alstom Technology Ltd	METHOD TO SWITCH A COMBUSTION DEVICE
DE102011118688A1 (en) *	2011-11-16	2013-05-16	Daimler Ag	Flow-driven device
DE102018123785B4 (en)	2018-09-26	2023-07-27	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Method of operating a gas turbine assembly and gas turbine assembly

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE2751743C2 (en) *	1977-11-19	1985-04-18	Pierburg Luftfahrtgeräte Union GmbH, 4040 Neuss	Method and control device for metering flowing media
US5052174A (en) *	1988-07-28	1991-10-01	Williams International Corporation	Continuous flow fuel control system
US4926629A (en) *	1988-10-28	1990-05-22	Allied-Signal Inc.	Low cost fuel supply system for gas turbine engines
JP2758301B2 (en) *	1991-11-29	1998-05-28	株式会社東芝	Gas turbine combustor
DE19620874A1 (en) *	1996-05-23	1997-11-27	Bmw Rolls Royce Gmbh	Fuel injection for a staged gas turbine combustor
US6209309B1 (en) *	1997-12-19	2001-04-03	Hamilton Sundstrand Corporation	Pulse width modulated fuel flow control for an engine
US5913807A (en) *	1998-03-30	1999-06-22	Williams International Corp. L.L.C.	Turbojet engine start system

2000
- 2000-04-28 SE SE0001552A patent/SE522267C2/en not_active IP Right Cessation
2001
- 2001-04-27 WO PCT/SE2001/000931 patent/WO2001083965A1/en active Application Filing
- 2001-04-27 GB GB0224080A patent/GB2376721B/en not_active Expired - Fee Related
- 2001-04-27 DE DE10196104T patent/DE10196104B8/en not_active Expired - Fee Related
- 2001-04-27 AU AU2001252845A patent/AU2001252845A1/en not_active Abandoned

Also Published As

Publication number	Publication date
DE10196104B4 (en)	2011-02-10
SE0001552L (en)	2001-10-29
GB2376721B (en)	2004-07-07
WO2001083965A1 (en)	2001-11-08
AU2001252845A1 (en)	2001-11-12
DE10196104T1 (en)	2003-04-30
GB2376721A (en)	2002-12-24
SE0001552D0 (en)	2000-04-28
DE10196104B8 (en)	2011-05-05
SE522267C2 (en)	2004-01-27

Similar Documents

Publication	Publication Date	Title
PL344339A1 (en)	2001-11-05	Gas turbine fuel injector
GB2361303B (en)	2004-10-20	Wall structure for a gas turbine engine combustor
GB9928242D0 (en)	2000-01-26	Combustion chamber for a gas turbine engine
PL340223A1 (en)	2001-01-15	Fuel injection nozzle a gas turbine engine
GB9921935D0 (en)	1999-11-17	A nacelle assembly for a gas turbine engine
GB0214783D0 (en)	2002-08-07	Reheat combustion system for a gas turbine
GB9608027D0 (en)	1996-06-19	Fuel system for a gas turbine engine
GB0116988D0 (en)	2001-09-05	A gas turbine engine blade containment assembly
EP1270872A4 (en)	2003-08-27	Gas turbine engine
GB0025878D0 (en)	2000-12-06	Gas turbine engine combustion system
GB2361033B (en)	2004-06-09	A gas turbine engine blade containment assembly
GB0004696D0 (en)	2000-04-19	Gas turbine engine
GB9727157D0 (en)	1998-02-25	Fuel system for a gas turbine engine
GB0008193D0 (en)	2000-05-24	A gas turbine engine blade containment assembly
EA199900537A3 (en)	2000-08-28	A gas turbine engine combustion system
GB9712947D0 (en)	1997-08-20	Fuel control system for a gas turbine engine
GB0004694D0 (en)	2000-04-19	Gas turbine engine
GB9714645D0 (en)	1997-09-17	Fuel metering arrangement for a gas turbine engine
GB2365926B (en)	2004-12-08	A gas turbine engine blade containment assembly
EP1326022A4 (en)	2004-11-17	Combustion gas seal for injector
GB2376721B (en)	2004-07-07	Fuel injection system for a gas turbine
GB2366599B (en)	2004-10-27	Gas turbine engine system
GB9923809D0 (en)	1999-12-08	A gas turbine engine
GB2365925B (en)	2005-02-23	A gas turbine engine blade containment assembly
GB0008189D0 (en)	2000-05-24	A gas turbine engine blade containment assembly

Legal Events

Date	Code	Title	Description
2008-04-23	732E	Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
2012-12-26	PCNP	Patent ceased through non-payment of renewal fee	Effective date: 20120427