GB2414770B - Fuel injection control system for a turbine engine - Google Patents

Fuel injection control system for a turbine engine

Info

Publication number: GB2414770B
Authority: GB; United Kingdom
Prior art keywords: control system; fuel injection; turbine engine; injection control; turbine
Prior art date: 2003-02-21
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

GB0519175A

Other versions

GB0519175D0 (en

GB2414770A (en

Inventor

Charles F Nearhoof Sr

Charles F Nearhoof Jr

Kevin P Pearce

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.)

TURBINE PROPERTIES LLC

Original Assignee

TURBINE PROPERTIES LLC

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.)

2003-02-21

Filing date

2003-02-21

Publication date

2006-08-09

2003-02-21 Application filed by TURBINE PROPERTIES LLC filed Critical TURBINE PROPERTIES LLC

2003-02-21 Priority claimed from PCT/US2003/005266 external-priority patent/WO2004076836A1/en

2005-10-26 Publication of GB0519175D0 publication Critical patent/GB0519175D0/en

2005-12-07 Publication of GB2414770A publication Critical patent/GB2414770A/en

2006-08-09 Application granted granted Critical

2006-08-09 Publication of GB2414770B publication Critical patent/GB2414770B/en

2023-02-21 Anticipated expiration legal-status Critical

Status Expired - Fee Related legal-status Critical Current

Links

239000000446 fuel Substances 0.000 title 1
238000002347 injection Methods 0.000 title 1
239000007924 injection Substances 0.000 title 1

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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- 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
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
- 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
- F23R7/00—Intermittent or explosive combustion chambers

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Output Control And Ontrol Of Special Type Engine (AREA)

GB0519175A 2003-02-21 2003-02-21 Fuel injection control system for a turbine engine Expired - Fee Related GB2414770B (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
PCT/US2003/005266 WO2004076836A1 (en)	2002-01-29	2003-02-21	Fuel injection control system for a turbine engine

Publications (3)

Publication Number	Publication Date
GB0519175D0 GB0519175D0 (en)	2005-10-26
GB2414770A GB2414770A (en)	2005-12-07
GB2414770B true GB2414770B (en)	2006-08-09

Family

ID=34374753

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
GB0519175A Expired - Fee Related GB2414770B (en)	2003-02-21	2003-02-21	Fuel injection control system for a turbine engine

Country Status (6)

Country	Link
AU (1)	AU2003213187A1 (en)
BR (1)	BR0318137A (en)
CA (1)	CA2516386A1 (en)
DE (1)	DE10394149T5 (en)
GB (1)	GB2414770B (en)
MX (1)	MXPA05008924A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2880760A (en) *	1956-08-24	1959-04-07	Bendix Aviat Corp	Harmonic exciter valve
US3688495A (en) *	1970-04-17	1972-09-05	Adolf Fehler	Control system for metering the fuel flow in gas turbine engines
US3738104A (en) *	1971-07-16	1973-06-12	Gen Electric	Gas turbine fuel flow metering control system
US3946551A (en) *	1974-01-17	1976-03-30	United Technologies Corporation	Pumping and metering system
US4454713A (en) *	1981-06-04	1984-06-19	Chandler Evans Inc.	Pulse width modulated fuel metering system
US4545198A (en) *	1982-08-10	1985-10-08	Nissan Motor Company, Limited	Gas turbine engine control system

2003
- 2003-02-21 GB GB0519175A patent/GB2414770B/en not_active Expired - Fee Related
- 2003-02-21 DE DE10394149T patent/DE10394149T5/en not_active Withdrawn
- 2003-02-21 MX MXPA05008924A patent/MXPA05008924A/en active IP Right Grant
- 2003-02-21 CA CA002516386A patent/CA2516386A1/en not_active Abandoned
- 2003-02-21 BR BR0318137-5A patent/BR0318137A/en not_active IP Right Cessation
- 2003-02-21 AU AU2003213187A patent/AU2003213187A1/en not_active Abandoned

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2880760A (en) *	1956-08-24	1959-04-07	Bendix Aviat Corp	Harmonic exciter valve
US3688495A (en) *	1970-04-17	1972-09-05	Adolf Fehler	Control system for metering the fuel flow in gas turbine engines
US3738104A (en) *	1971-07-16	1973-06-12	Gen Electric	Gas turbine fuel flow metering control system
US3946551A (en) *	1974-01-17	1976-03-30	United Technologies Corporation	Pumping and metering system
US4454713A (en) *	1981-06-04	1984-06-19	Chandler Evans Inc.	Pulse width modulated fuel metering system
US4545198A (en) *	1982-08-10	1985-10-08	Nissan Motor Company, Limited	Gas turbine engine control system

Also Published As

Publication number	Publication date
CA2516386A1 (en)	2004-09-10
MXPA05008924A (en)	2006-05-25
AU2003213187A1 (en)	2004-09-17
DE10394149T5 (en)	2007-08-09
GB0519175D0 (en)	2005-10-26
BR0318137A (en)	2006-02-07
GB2414770A (en)	2005-12-07

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Legal Events

Date	Code	Title	Description
2008-10-29	PCNP	Patent ceased through non-payment of renewal fee	Effective date: 20080221