FR2018565A1 - - Google Patents
Info
- Publication number
- FR2018565A1 FR2018565A1 FR6932136A FR6932136A FR2018565A1 FR 2018565 A1 FR2018565 A1 FR 2018565A1 FR 6932136 A FR6932136 A FR 6932136A FR 6932136 A FR6932136 A FR 6932136A FR 2018565 A1 FR2018565 A1 FR 2018565A1
- 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.)
- Withdrawn
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
- F23R3/06—Arrangement of apertures along the flame tube
-
- 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
-
- 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
- F23R3/26—Controlling the air flow
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)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB44805/68A GB1278590A (en) | 1968-09-20 | 1968-09-20 | Combustion chambers for gas turbine engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR2018565A1 true FR2018565A1 (en) | 1970-05-29 |
Family
ID=10434833
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR6932136A Withdrawn FR2018565A1 (en) | 1968-09-20 | 1969-09-22 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3593518A (en) |
| FR (1) | FR2018565A1 (en) |
| GB (1) | GB1278590A (en) |
| SE (1) | SE357028B (en) |
Families Citing this family (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3859786A (en) * | 1972-05-25 | 1975-01-14 | Ford Motor Co | Combustor |
| US3814575A (en) * | 1973-04-25 | 1974-06-04 | Us Air Force | Combustion device |
| US4021186A (en) * | 1974-06-19 | 1977-05-03 | Exxon Research And Engineering Company | Method and apparatus for reducing NOx from furnaces |
| GB1481617A (en) * | 1974-10-07 | 1977-08-03 | Rolls Royce | Gas turbine fuel burners |
| DE2452178C3 (en) * | 1974-11-02 | 1981-05-07 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Combustion chamber for gas turbine engines |
| DE2545234C2 (en) * | 1975-10-09 | 1983-09-15 | Fa. J. Eberspächer, 7300 Esslingen | Mixing device for burners |
| US4052144A (en) * | 1976-03-31 | 1977-10-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Fuel combustor |
| DE2839627C2 (en) * | 1977-09-13 | 1983-11-03 | Hitachi, Ltd., Tokyo | Gas burner |
| US4276018A (en) * | 1979-05-30 | 1981-06-30 | Davey Compressor Co. | Mobile heater |
| US5109671A (en) * | 1989-12-05 | 1992-05-05 | Allied-Signal Inc. | Combustion apparatus and method for a turbine engine |
| FR2674317B1 (en) * | 1991-03-20 | 1993-05-28 | Snecma | COMBUSTION CHAMBER OF A TURBOMACHINE COMPRISING AN ADJUSTMENT OF THE FUEL FLOW. |
| US5289686A (en) * | 1992-11-12 | 1994-03-01 | General Motors Corporation | Low nox gas turbine combustor liner with elliptical apertures for air swirling |
| US5322026A (en) * | 1992-12-21 | 1994-06-21 | Bay Il H | Waste combustion chamber with tertiary burning zone |
| GB9726697D0 (en) | 1997-12-18 | 1998-02-18 | Secr Defence | Fuel injector |
| US20060130486A1 (en) * | 2004-12-17 | 2006-06-22 | Danis Allen M | Method and apparatus for assembling gas turbine engine combustors |
| DE102006041955A1 (en) * | 2006-08-30 | 2008-03-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method for controlling combustion in a combustion chamber and combustion chamber device |
| US8171740B2 (en) * | 2009-02-27 | 2012-05-08 | Honeywell International Inc. | Annular rich-quench-lean gas turbine combustors with plunged holes |
| US8141365B2 (en) * | 2009-02-27 | 2012-03-27 | Honeywell International Inc. | Plunged hole arrangement for annular rich-quench-lean gas turbine combustors |
| US20100242483A1 (en) * | 2009-03-30 | 2010-09-30 | United Technologies Corporation | Combustor for gas turbine engine |
| US9222674B2 (en) * | 2011-07-21 | 2015-12-29 | United Technologies Corporation | Multi-stage amplification vortex mixture for gas turbine engine combustor |
| CN103032891B (en) * | 2013-01-04 | 2015-07-29 | 中国科学院工程热物理研究所 | A kind of many eddy combustion methods |
| US20140190171A1 (en) * | 2013-01-10 | 2014-07-10 | Honeywell International Inc. | Combustors with hybrid walled liners |
| CA2820365C (en) * | 2013-06-25 | 2021-03-23 | Unique Gas Products Ltd. | Direct venting system for free-standing propane powered absorption refrigerator |
| EP3039340B1 (en) * | 2013-08-30 | 2018-11-28 | United Technologies Corporation | Vena contracta swirling dilution passages for gas turbine engine combustor |
| US11112115B2 (en) * | 2013-08-30 | 2021-09-07 | Raytheon Technologies Corporation | Contoured dilution passages for gas turbine engine combustor |
| US10451281B2 (en) * | 2014-11-04 | 2019-10-22 | United Technologies Corporation | Low lump mass combustor wall with quench aperture(s) |
| DE102016201452A1 (en) * | 2016-02-01 | 2017-08-03 | Rolls-Royce Deutschland Ltd & Co Kg | Gas turbine combustor with wall contouring |
| US20180283695A1 (en) * | 2017-04-03 | 2018-10-04 | United Technologies Corporation | Combustion panel grommet |
| US11959643B2 (en) * | 2021-06-07 | 2024-04-16 | General Electric Company | Combustor for a gas turbine engine |
| US12222104B2 (en) * | 2022-03-21 | 2025-02-11 | General Electric Company | Turbine engine combustor and combustor liner |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB738006A (en) * | 1952-07-12 | 1955-10-05 | Rolls Royce | Improvements in or relating to gas turbine engines |
| US2807933A (en) * | 1954-04-01 | 1957-10-01 | Martin Peter | Combustion chambers |
| US2841182A (en) * | 1955-12-29 | 1958-07-01 | Westinghouse Electric Corp | Boundary layer fluid control apparatus |
| GB1075958A (en) * | 1966-04-29 | 1967-07-19 | Rolls Royce | Gas turbine engine |
-
1968
- 1968-09-20 GB GB44805/68A patent/GB1278590A/en not_active Expired
-
1969
- 1969-09-17 US US858770A patent/US3593518A/en not_active Expired - Lifetime
- 1969-09-19 SE SE12892/69A patent/SE357028B/xx unknown
- 1969-09-22 FR FR6932136A patent/FR2018565A1/fr not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| DE1947762A1 (en) | 1970-04-02 |
| GB1278590A (en) | 1972-06-21 |
| SE357028B (en) | 1973-06-12 |
| US3593518A (en) | 1971-07-20 |
| DE1947762B2 (en) | 1975-07-24 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |