GB8803121D0 - Gas turbine engine with augmentor & variable area bypass injector - Google Patents

Gas turbine engine with augmentor & variable area bypass injector

Info

Publication number: GB8803121D0
Authority: GB; United Kingdom
Prior art keywords: augmentor; gas turbine; turbine engine; variable area; area bypass
Prior art date: 1987-02-13
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

GB888803121A

Other versions

GB2202589B (en

GB2202589A (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.)

General Electric Co

Original Assignee

General Electric Co

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.)

1987-02-13

Filing date

1988-02-11

Publication date

1988-03-09

1988-02-11 Application filed by General Electric Co filed Critical General Electric Co

1988-03-09 Publication of GB8803121D0 publication Critical patent/GB8803121D0/en

1988-09-28 Publication of GB2202589A publication Critical patent/GB2202589A/en

1991-10-02 Application granted granted Critical

1991-10-02 Publication of GB2202589B publication Critical patent/GB2202589B/en

2008-02-11 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
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/38—Introducing air inside the jet
- F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary 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
- F23R3/02—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
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
- F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Turbine Rotor Nozzle Sealing (AREA)
Pre-Mixing And Non-Premixing Gas Burner (AREA)
Separation By Low-Temperature Treatments (AREA)
Combustion Of Fluid Fuel (AREA)

GB8803121A 1987-02-13 1988-02-11 Gas turbine engine with augmentor and variable area bypass injector Expired - Fee Related GB2202589B (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US1456287A	1987-02-13	1987-02-13

Publications (3)

Publication Number	Publication Date
GB8803121D0 true GB8803121D0 (en)	1988-03-09
GB2202589A GB2202589A (en)	1988-09-28
GB2202589B GB2202589B (en)	1991-10-02

Family

ID=21766218

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
GB8803121A Expired - Fee Related GB2202589B (en)	1987-02-13	1988-02-11	Gas turbine engine with augmentor and variable area bypass injector

Country Status (5)

Country	Link
JP (1)	JPS63227930A (en)
DE (1)	DE3803992A1 (en)
FR (1)	FR2610994B1 (en)
GB (1)	GB2202589B (en)
SE (1)	SE466559B (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE8915860U1 (en) *	1989-02-08	1991-12-05	Deutsche Forschungsanstalt für Luft- und Raumfahrt eV, 5300 Bonn	Jet engine
US5261229A (en) *	1992-08-03	1993-11-16	General Electric Company	Noise-suppressed exhaust nozzles for jet engines
FR2712962B1 (en) *	1993-11-24	1995-12-29	Snecma	Post-combustion device comprising an improved flame catching device.
FR2763648B1 (en) *	1997-05-22	1999-07-02	Snecma	DICHOTOMIC HEATING SYSTEM REDUCING DRY LOSSES
US7596950B2 (en) *	2005-09-16	2009-10-06	General Electric Company	Augmentor radial fuel spray bar with counterswirling heat shield
US7603863B2 (en) *	2006-06-05	2009-10-20	General Electric Company	Secondary fuel injection from stage one nozzle
JP5625585B2 (en) *	2010-07-27	2014-11-19	株式会社Ihi	Afterburner and aircraft engine
JP6229590B2 (en)	2014-04-30	2017-11-15	株式会社Ihi	Afterburner and aircraft engine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3060680A (en) *	1957-12-30	1962-10-30	Rolls Royce	By-pass gas-turbine engine and control therefor
GB928475A (en) *	1961-12-27	1963-06-12	Rolls Royce	Improvements in or relating to by-pass gas turbine engines
GB1029900A (en) *	1964-11-27	1966-05-18	Rolls Royce	By-pass gas turbine jet engine
DE1923150A1 (en) *	1968-05-08	1970-01-15	Man Turbo Gmbh	Turbine jet engine
US4335573A (en) *	1970-09-02	1982-06-22	General Electric Company	Gas turbine engine mixer
US3698186A (en) *	1970-12-24	1972-10-17	United Aircraft Corp	Afterburner combustion apparatus
BE795529A (en) *	1972-02-17	1973-06-18	Gen Electric	IGNITER MOUNTED ON A TURBOREACTOR THRUST INCREASING DEVICE AND AIR COOLED
US4072008A (en) *	1976-05-04	1978-02-07	General Electric Company	Variable area bypass injector system
JPS5641815A (en) *	1979-09-12	1981-04-18	Mitsui Toatsu Chem Inc	Purifying method for wet process phosphoric acid solution
US4461146A (en) *	1982-10-22	1984-07-24	The United States Of America As Represented By The Secretary Of The Navy	Mixed flow swirl augmentor for turbofan engine

1988
- 1988-02-04 FR FR8801282A patent/FR2610994B1/en not_active Expired - Lifetime
- 1988-02-10 DE DE19883803992 patent/DE3803992A1/en not_active Withdrawn
- 1988-02-11 GB GB8803121A patent/GB2202589B/en not_active Expired - Fee Related
- 1988-02-11 SE SE8800465A patent/SE466559B/en not_active IP Right Cessation
- 1988-02-12 JP JP2905188A patent/JPS63227930A/en active Granted

Also Published As

Publication number	Publication date
JPH0587652B2 (en)	1993-12-17
FR2610994B1 (en)	1993-06-11
SE8800465D0 (en)	1988-02-11
FR2610994A1 (en)	1988-08-19
GB2202589B (en)	1991-10-02
SE8800465L (en)	1988-08-14
GB2202589A (en)	1988-09-28
SE466559B (en)	1992-03-02
JPS63227930A (en)	1988-09-22
DE3803992A1 (en)	1988-08-25

Publication	Publication Date	Title
GB2206686B (en)	1989-11-22	Gas turbine engine augmentor
GB2055186B (en)	1983-05-25	Gas turbine engine dual fuel injector
GB2218741B (en)	1993-01-06	Gas turbine engine
GB8630754D0 (en)	1987-02-04	Turbofan gas turbine engine
GB8624163D0 (en)	1986-11-12	Turbofan gas turbine engine
GB8616153D0 (en)	1986-12-17	Turbofan gas turbine engine
GB8819537D0 (en)	1988-09-21	Combustion chamber for gas turbine engine
GB2182724B (en)	1988-12-07	Gas turbine engine thrust reverser
GB2207191B (en)	1992-03-04	Gas turbine engine
GB2219045B (en)	1992-06-03	Gas turbine engine fuel system
GB8911806D0 (en)	1989-07-12	Gas turbine engine fuel control system with enhanced relight capability
GB8700806D0 (en)	1987-02-18	Turbopropeller/gas turbine engine
GB2102936B (en)	1985-02-13	Fuel injector for gas turbine engines
GB8823360D0 (en)	1988-11-09	Fuel nozzle assembly for gas turbine engine
GB2238864B (en)	1992-04-22	Gas turbine engine combustors
GB2175992B (en)	1988-12-21	Gas turbine engine gaseous fuel injector
GB2193999B (en)	1990-08-29	Gas turbine engine with variable bypass means
IL83766A (en)	1991-03-10	Augmentor liner construction for gas turbine engine
GB2035540B (en)	1983-02-09	Gas turbine engine fuel injector
IL80634A0 (en)	1987-02-27	Gas turbine engine augmentor
GB8803121D0 (en)	1988-03-09	Gas turbine engine with augmentor & variable area bypass injector
GB8830151D0 (en)	1989-02-22	Gas turbine engine
GB8616154D0 (en)	1986-12-17	Turbofan gas turbine engine
GB8703101D0 (en)	1987-03-18	Gas turbine engine combustion chambers
JPS56168037A (en)	1981-12-24	Fuel injector for gas turbine engine

Legal Events

Date	Code	Title	Description
1994-10-05	PCNP	Patent ceased through non-payment of renewal fee	Effective date: 19940211