FR2608258B1 - Dispositif de combustion pour un moteur a turbine a gaz - Google Patents

Dispositif de combustion pour un moteur a turbine a gaz

Info

Publication number: FR2608258B1
Authority: FR; France
Prior art keywords: gas turbine; turbine engine; combustion device; combustion; engine
Prior art date: 1986-12-10
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

FR8717211A

Other languages

English (en)

Other versions

FR2608258A1 (fr

Inventor

Douglas Willis Jeffrey

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.)

1986-12-10

Filing date

1987-12-10

Publication date

1994-02-25

1987-12-10 Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC

1988-06-17 Publication of FR2608258A1 publication Critical patent/FR2608258A1/fr

1994-02-25 Application granted granted Critical

1994-02-25 Publication of FR2608258B1 publication Critical patent/FR2608258B1/fr

2007-12-10 Anticipated expiration legal-status Critical

Status Expired - Fee Related legal-status Critical Current

Links

238000002485 combustion reaction Methods 0.000 title 1
RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1

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
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Output Control And Ontrol Of Special Type Engine (AREA)
Engine Equipment That Uses Special Cycles (AREA)

FR8717211A 1986-12-10 1987-12-10 Dispositif de combustion pour un moteur a turbine a gaz Expired - Fee Related FR2608258B1 (fr)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
GB8629468A GB2198518B (en)	1986-12-10	1986-12-10	Combustion apparatus for a gas turbine engine

Publications (2)

Publication Number	Publication Date
FR2608258A1 FR2608258A1 (fr)	1988-06-17
FR2608258B1 true FR2608258B1 (fr)	1994-02-25

Family

ID=10608742

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR8717211A Expired - Fee Related FR2608258B1 (fr)	1986-12-10	1987-12-10	Dispositif de combustion pour un moteur a turbine a gaz

Country Status (5)

Country	Link
US (1)	US4893475A (fr)
JP (1)	JP2617495B2 (fr)
DE (1)	DE3741021C2 (fr)
FR (1)	FR2608258B1 (fr)
GB (1)	GB2198518B (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US5121608A (en) *	1988-02-06	1992-06-16	Rolls-Royce Plc	Gas turbine engine fuel burner
US5996351A (en) *	1997-07-07	1999-12-07	General Electric Company	Rapid-quench axially staged combustor
GB9811577D0 (en) *	1998-05-30	1998-07-29	Rolls Royce Plc	A fuel injector
US6260359B1 (en) *	1999-11-01	2001-07-17	General Electric Company	Offset dilution combustor liner
US6928822B2 (en) *	2002-05-28	2005-08-16	Lytesyde, Llc	Turbine engine apparatus and method
US7926284B2 (en) *	2006-11-30	2011-04-19	Honeywell International Inc.	Quench jet arrangement for annular rich-quench-lean gas turbine combustors
US8127554B2 (en) *	2007-11-29	2012-03-06	Honeywell International Inc.	Quench jet arrangement for annular rich-quench-lean gas turbine combustors
US8616004B2 (en) *	2007-11-29	2013-12-31	Honeywell International Inc.	Quench jet arrangement for annular rich-quench-lean gas turbine combustors
FR2982010B1 (fr) *	2011-10-26	2013-11-08	Snecma	Chambre de combustion annulaire dans une turbomachine
US9121613B2 (en) *	2012-06-05	2015-09-01	General Electric Company	Combustor with brief quench zone with slots
CN106907740B (zh) *	2013-10-18	2019-07-05	三菱重工业株式会社	燃料喷射器

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB1136543A (en) *	1966-02-21	1968-12-11	Rolls Royce	Liquid fuel combustion apparatus for gas turbine engines
DE1934700B2 (de) *	1969-07-09	1972-01-05	Mtu Muenchen Gmbh	Brennstoffduese fuer gasturbinentriebwerke
US3703259A (en) *	1971-05-03	1972-11-21	Gen Electric	Air blast fuel atomizer
US3724207A (en) *	1971-08-05	1973-04-03	Gen Motors Corp	Combustion apparatus
GB1427146A (en) *	1972-09-07	1976-03-10	Rolls Royce	Combustion apparatus for gas turbine engines
US3961475A (en) *	1972-09-07	1976-06-08	Rolls-Royce (1971) Limited	Combustion apparatus for gas turbine engines
US4078377A (en) *	1974-01-28	1978-03-14	Ford Motor Company	Internally vaporizing low emission combustor
GB2040434A (en) *	1978-03-14	1980-08-28	Rolls Royce	Gas Turbine Engine Combustion Equipment
GB2021204B (en) *	1978-05-20	1982-10-13	Rolls Royce	Gas turbinr combustion chamber
GB2055187B (en) *	1979-08-01	1983-12-14	Rolls Royce	Gaseous fuel injector for a gas turbine engine
GB2119077B (en) *	1982-04-22	1985-08-14	Rolls Royce	Fuel injector for gas turbine engines

1986
- 1986-12-10 GB GB8629468A patent/GB2198518B/en not_active Expired - Fee Related
1987
- 1987-12-03 DE DE3741021A patent/DE3741021C2/de not_active Expired - Fee Related
- 1987-12-04 JP JP62307347A patent/JP2617495B2/ja not_active Expired - Lifetime
- 1987-12-10 FR FR8717211A patent/FR2608258B1/fr not_active Expired - Fee Related
1989
- 1989-07-17 US US07/380,749 patent/US4893475A/en not_active Expired - Lifetime

Also Published As

Publication number	Publication date
FR2608258A1 (fr)	1988-06-17
JPS63150515A (ja)	1988-06-23
DE3741021C2 (de)	1998-07-23
DE3741021A1 (de)	1988-06-23
GB8629468D0 (en)	1987-01-21
US4893475A (en)	1990-01-16
GB2198518B (en)	1990-08-01
JP2617495B2 (ja)	1997-06-04
GB2198518A (en)	1988-06-15

Similar Documents

Publication	Publication Date	Title
FR2586453B1 (fr)	1992-11-06	Carburateur pour moteur a turbine a gaz
FR2583459B1 (fr)	1992-08-07	Dispositif de regulation de carburant pour un moteur a turbine a gaz.
FR2554170B1 (fr)	1987-11-20	Systeme de combustion pour moteur a turbine a gaz
FR2594886B1 (fr)	1990-09-07	Module propulsif pour un moteur aeronautique a turbine a gaz
FR2475119B1 (fr)	1986-08-22	Dispositif de reglage de l'emission des gaz d'echappement pour moteur diesel
FR2406726B1 (fr)	1985-11-29	Appareillage de combustion perfectionne pour moteur a turbine a gaz
FR2617907B1 (fr)	1994-04-08	Moteur a turbine a gaz
FR2557212B1 (fr)	1986-12-19	Structure de stator pour un moteur a turbine a gaz
FR2632015B1 (fr)	1993-10-08	Syste me d'injecteurs pour moteur a turbine a gaz
FR2578582B1 (fr)	1989-06-02	Dispositif de commande de clapet de moteur a turbine a gaz
FR2580725B1 (fr)	1991-05-10	Module propulsif pour un moteur a turbine a gaz aeronautique
FR2515735B1 (fr)	1988-09-23	Dispositif de suppression de rayonnement infrarouge pour moteur a turbine a gaz
FR2586755B1 (fr)	1994-03-11	Systeme de carburant pour un moteur a turbine a gaz
FR2632014B1 (fr)	1994-05-27	Injecteur de carburant pour moteur a turbine a gaz
FR2594180B1 (fr)	1989-01-13	Dispositif de demarrage a air comprime pour moteurs a combustion interne
GB2150277B (en)	1987-01-28	Combustion apparatus for a gas turbine engine
FR2510665B1 (fr)	1989-02-10	Injecteur mixte de carburant pour moteur a turbine a gaz
FR2589427B1 (fr)	1992-01-24	Module d'helice pour un moteur a turbine a gaz aeronautique
FR2527268B1 (fr)	1988-09-09	Prediffuseur pour un moteur a turbine a gaz
FR2601068B1 (fr)	1993-05-28	Turbine de puissance pour moteur a turbine a gaz.
FR2475628B1 (fr)	1986-05-23	Entree d'air a dispositif epurateur pour moteur a turbine a gaz
FR2460390B1 (fr)	1986-02-07	Diffuseur pour moteur a turbine a gaz
FR2649445B1 (fr)	1991-10-04	Dispositif de decharge pour moteur de turbine a gaz a double flux
FR2512500B1 (fr)	1987-08-14	Dispositif d'alimentation en combustible pour moteurs a allumage par compression
FR2476230B1 (fr)	1985-07-19	Systeme d'injection de carburant pour augmentateur de poussee de moteur a turbine a gaz

Legal Events

Date	Code	Title	Description
2000-10-13	ST	Notification of lapse