FR2188055B1 - - Google Patents

Info

Publication number: FR2188055B1
Authority: FR; France
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

Application number

FR7321313A

Other languages

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.)

ZF International UK Ltd

Original Assignee

Lucas Industries Ltd

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.)

1972-06-09

Filing date

1973-06-12

Publication date

1976-09-17

1973-06-12 Application filed by Lucas Industries Ltd filed Critical Lucas Industries Ltd

1974-01-18 Publication of FR2188055A1 publication Critical patent/FR2188055A1/fr

1976-09-17 Application granted granted Critical

1976-09-17 Publication of FR2188055B1 publication Critical patent/FR2188055B1/fr

Status Expired legal-status Critical Current

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
- F23R3/02—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
- 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)
Pre-Mixing And Non-Premixing Gas Burner (AREA)
Gas Burners (AREA)

FR7321313A 1972-06-09 1973-06-12 Expired FR2188055B1 (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
GB2715472A GB1424197A (en)	1972-06-09	1972-06-09	Combustion chambers for gas turbine engines

Publications (2)

Publication Number	Publication Date
FR2188055A1 FR2188055A1 (en)	1974-01-18
FR2188055B1 true FR2188055B1 (en)	1976-09-17

Family

ID=10255088

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR7321313A Expired FR2188055B1 (en)	1972-06-09	1973-06-12

Country Status (6)

Country	Link
US (1)	US3869864A (en)
JP (1)	JPS5411844B2 (en)
DE (1)	DE2329367C2 (en)
FR (1)	FR2188055B1 (en)
GB (1)	GB1424197A (en)
IT (1)	IT989653B (en)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB1552132A (en) *	1975-11-29	1979-09-12	Rolls Royce	Combustion chambers for gas turbine engines
JPS5638389Y2 (en) *	1976-12-09	1981-09-08
GB1571213A (en) *	1977-01-28	1980-07-09	Kainov G	Combustion chamber for gas turbine engine
DE2723546A1 (en) *	1977-05-25	1978-11-30	Motoren Turbinen Union	COMBUSTION CHAMBER, IN PARTICULAR REVERSAL COMBUSTION CHAMBER FOR GAS TURBINE ENGINES
DE2728399C2 (en) *	1977-06-24	1982-04-22	Brown, Boveri & Cie Ag, 6800 Mannheim	Combustion chamber for a gas turbine
US4195476A (en) *	1978-04-27	1980-04-01	General Motors Corporation	Combustor construction
US4361010A (en) *	1980-04-02	1982-11-30	United Technologies Corporation	Combustor liner construction
US4765136A (en) *	1985-11-25	1988-08-23	United Technologies Corporation	Gas turbine engine augmentor
US4928479A (en) *	1987-12-28	1990-05-29	Sundstrand Corporation	Annular combustor with tangential cooling air injection
US4944152A (en) *	1988-10-11	1990-07-31	Sundstrand Corporation	Augmented turbine combustor cooling
US4949545A (en) *	1988-12-12	1990-08-21	Sundstrand Corporation	Turbine wheel and nozzle cooling
US5109671A (en) *	1989-12-05	1992-05-05	Allied-Signal Inc.	Combustion apparatus and method for a turbine engine
JPH0387059U (en) *	1989-12-11	1991-09-04
US5069033A (en) *	1989-12-21	1991-12-03	Sundstrand Corporation	Radial inflow combustor
US5113647A (en) *	1989-12-22	1992-05-19	Sundstrand Corporation	Gas turbine annular combustor
US5165226A (en) *	1991-08-09	1992-11-24	Pratt & Whitney Canada, Inc.	Single vortex combustor arrangement
US5237813A (en) *	1992-08-21	1993-08-24	Allied-Signal Inc.	Annular combustor with outer transition liner cooling
US5271220A (en) *	1992-10-16	1993-12-21	Sundstrand Corporation	Combustor heat shield for a turbine containment ring
US5746048A (en) *	1994-09-16	1998-05-05	Sundstrand Corporation	Combustor for a gas turbine engine
US5628193A (en) *	1994-09-16	1997-05-13	Alliedsignal Inc.	Combustor-to-turbine transition assembly
US6079199A (en) *	1998-06-03	2000-06-27	Pratt & Whitney Canada Inc.	Double pass air impingement and air film cooling for gas turbine combustor walls
EP1295018A4 (en)	2000-05-01	2004-06-02	Elliott Energy Systems Inc	Annular combustor for use with an energy system
US6405703B1 (en)	2001-06-29	2002-06-18	Brian Sowards	Internal combustion engine
US6925810B2 (en) *	2002-11-08	2005-08-09	Honeywell International, Inc.	Gas turbine engine transition liner assembly and repair
US7308794B2 (en) *	2004-08-27	2007-12-18	Pratt & Whitney Canada Corp.	Combustor and method of improving manufacturing accuracy thereof
DE102005008421A1 (en) *	2005-02-24	2006-08-31	Alstom Technology Ltd.	Combustion chamber for a gas turbine, at a power station, has an additional air jet to give a counter flow and increase the fuel/air recirculation within the combustion zone
DE112006000934T5 (en) *	2005-04-13	2008-06-05	Corning Inc.	Mode matching system for lasers with tunable external resonator
US7954326B2 (en) *	2007-11-28	2011-06-07	Honeywell International Inc.	Systems and methods for cooling gas turbine engine transition liners
WO2010096817A2 (en)	2009-02-23	2010-08-26	Williams International Co., L.L.C.	Combustion system
US8864492B2 (en) *	2011-06-23	2014-10-21	United Technologies Corporation	Reverse flow combustor duct attachment
US9879862B2 (en)	2013-03-08	2018-01-30	Rolls-Royce North American Technologies, Inc.	Gas turbine engine afterburner
US20150323185A1 (en)	2014-05-07	2015-11-12	General Electric Compamy	Turbine engine and method of assembling thereof
US11674446B2 (en) *	2021-08-30	2023-06-13	Collins Engine Nozzles, Inc.	Cooling for surface ignitors in torch ignition devices
US11674445B2 (en) *	2021-08-30	2023-06-13	Collins Engine Nozzles, Inc.	Cooling for continuous ignition devices
US20230296250A1 (en) *	2022-03-21	2023-09-21	General Electric Company	Turbine engine combustor and combustor liner

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2531810A (en) *	1946-06-05	1950-11-28	Kellogg M W Co	Air inlet arrangement for combustion chamber flame tubes
BE507258A (en) *	1950-12-02
US3333414A (en) *	1965-10-13	1967-08-01	United Aircraft Canada	Aerodynamic-flow reverser and smoother
GB1289523A (en) *	1969-03-17	1972-09-20
US3613360A (en) *	1969-10-30	1971-10-19	Garrett Corp	Combustion chamber construction
US3653207A (en) *	1970-07-08	1972-04-04	Gen Electric	High fuel injection density combustion chamber for a gas turbine engine
US3671171A (en) *	1970-11-27	1972-06-20	Avco Corp	Annular combustors

1972
- 1972-06-09 GB GB2715472A patent/GB1424197A/en not_active Expired
1973
- 1973-06-07 IT IT50516/73A patent/IT989653B/en active
- 1973-06-08 DE DE2329367A patent/DE2329367C2/en not_active Expired
- 1973-06-09 JP JP6529173A patent/JPS5411844B2/ja not_active Expired
- 1973-06-11 US US368576A patent/US3869864A/en not_active Expired - Lifetime
- 1973-06-12 FR FR7321313A patent/FR2188055B1/fr not_active Expired

Also Published As

Publication number	Publication date
FR2188055A1 (en)	1974-01-18
JPS4949012A (en)	1974-05-13
GB1424197A (en)	1976-02-11
US3869864A (en)	1975-03-11
DE2329367C2 (en)	1981-12-24
IT989653B (en)	1975-06-10
JPS5411844B2 (en)	1979-05-18
DE2329367A1 (en)	1973-12-20

Publication	Publication Date	Title
FR2188055B1 (en)	1976-09-17
JPS5242939B2 (en)	1977-10-27
JPS4930651A (en)	1974-03-19
JPS4978530A (en)	1974-07-29
JPS5346552Y2 (en)	1978-11-08
JPS5234091B2 (en)	1977-09-01
JPS4893002U (en)	1973-11-07
JPS4961927U (en)	1974-05-30
JPS4966665A (en)	1974-06-27
CH557907A (en)	1975-01-15
BG18658A1 (en)	1975-03-20
CH567911A5 (en)	1975-10-15
CH571657A5 (en)	1976-01-15
CH578837A5 (en)	1976-08-31
CH563063A5 (en)	1975-06-13
CH559981A5 (en)	1975-03-14
CH559685A5 (en)	1975-03-14
CH559672A5 (en)	1975-03-14
CH559524A5 (en)	1975-03-14
CH569057A5 (en)	1975-11-14
CH606470A5 (en)	1978-10-31
BG21461A1 (en)	1976-07-20
CH569289A5 (en)	1975-11-14
CH570116A5 (en)	1975-12-15
CH570148A5 (en)	1975-12-15

Legal Events

Date	Code	Title
1975-12-12	TP	Transmission of property
1976-02-06	CD	Change of name or company name
1990-04-27	ST	Notification of lapse