FR2188055A1 - - Google Patents

Info

Publication number
FR2188055A1
FR2188055A1 FR7321313A FR7321313A FR2188055A1 FR 2188055 A1 FR2188055 A1 FR 2188055A1 FR 7321313 A FR7321313 A FR 7321313A FR 7321313 A FR7321313 A FR 7321313A FR 2188055 A1 FR2188055 A1 FR 2188055A1
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.)
Granted
Application number
FR7321313A
Other languages
French (fr)
Other versions
FR2188055B1 (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.)
Northrop Grumman Properties Ltd
Original Assignee
Lucas Aerospace 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.)
Filing date
Publication date
Application filed by Lucas Aerospace Ltd filed Critical Lucas Aerospace Ltd
Publication of FR2188055A1 publication Critical patent/FR2188055A1/fr
Application granted granted Critical
Publication of FR2188055B1 publication Critical patent/FR2188055B1/fr
Expired legal-status Critical Current

Links

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
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 true FR2188055A1 (en) 1974-01-18
FR2188055B1 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)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0528297A1 (en) * 1991-08-09 1993-02-24 United Technologies Corporation Single vortex combustor arrangement
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

Families Citing this family (33)

* 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
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
CN1502007A (en) * 2000-05-01 2004-06-02 艾略特能源系统股份有限公司 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
WO2006112971A2 (en) * 2005-04-13 2006-10-26 Corning Incorporated Mode-matching system for tunable external cavity laser
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

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0528297A1 (en) * 1991-08-09 1993-02-24 United Technologies Corporation Single vortex combustor arrangement
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

Also Published As

Publication number Publication date
DE2329367A1 (en) 1973-12-20
GB1424197A (en) 1976-02-11
DE2329367C2 (en) 1981-12-24
FR2188055B1 (en) 1976-09-17
JPS5411844B2 (en) 1979-05-18
US3869864A (en) 1975-03-11
IT989653B (en) 1975-06-10
JPS4949012A (en) 1974-05-13

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Legal Events

Date Code Title Description
TP Transmission of property
CD Change of name or company name
ST Notification of lapse