CA1028511A - Gas turbine engine combustor having staged premixing tubes - Google Patents
Gas turbine engine combustor having staged premixing tubesInfo
- Publication number
- CA1028511A CA1028511A CA234,329A CA234329A CA1028511A CA 1028511 A CA1028511 A CA 1028511A CA 234329 A CA234329 A CA 234329A CA 1028511 A CA1028511 A CA 1028511A
- Authority
- CA
- Canada
- Prior art keywords
- gas turbine
- turbine engine
- engine combustor
- premixing tubes
- staged
- Prior art date
- 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
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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
-
- 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
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- 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
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Incineration Of Waste (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US501739A US3905192A (en) | 1974-08-29 | 1974-08-29 | Combustor having staged premixing tubes |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1028511A true CA1028511A (en) | 1978-03-28 |
Family
ID=23994832
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA234,329A Expired CA1028511A (en) | 1974-08-29 | 1975-08-26 | Gas turbine engine combustor having staged premixing tubes |
Country Status (9)
Country | Link |
---|---|
US (1) | US3905192A (de) |
JP (1) | JPS5185033A (de) |
CA (1) | CA1028511A (de) |
DE (1) | DE2538512A1 (de) |
FR (1) | FR2283321A1 (de) |
GB (1) | GB1489496A (de) |
IN (1) | IN142712B (de) |
IT (1) | IT1042151B (de) |
SE (1) | SE7509617L (de) |
Families Citing this family (53)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4012904A (en) * | 1975-07-17 | 1977-03-22 | Chrysler Corporation | Gas turbine burner |
GB1578474A (en) * | 1976-06-21 | 1980-11-05 | Gen Electric | Combustor mounting arrangement |
US4180974A (en) * | 1977-10-31 | 1980-01-01 | General Electric Company | Combustor dome sleeve |
IT1111808B (it) * | 1978-03-28 | 1986-01-13 | Rolls Royce | Perfezionamenti apportati ai dispositivi di combustione di motori a turbina a gas |
GB2044431B (en) * | 1979-03-20 | 1983-03-16 | Rolls Royce | Gas turbine |
GB2055187B (en) * | 1979-08-01 | 1983-12-14 | Rolls Royce | Gaseous fuel injector for a gas turbine engine |
FR2465080A1 (fr) * | 1979-09-17 | 1981-03-20 | Snecma | Dispositif de suspension aval de chambre de combustion pour turbomachines |
GB2109532B (en) * | 1981-11-07 | 1985-01-03 | Rolls Royce | Gas fuel injector |
US4606190A (en) * | 1982-07-22 | 1986-08-19 | United Technologies Corporation | Variable area inlet guide vanes |
US4497170A (en) * | 1982-07-22 | 1985-02-05 | The Garrett Corporation | Actuation system for a variable geometry combustor |
US4532762A (en) * | 1982-07-22 | 1985-08-06 | The Garrett Corporation | Gas turbine engine variable geometry combustor apparatus |
DE3241162A1 (de) * | 1982-11-08 | 1984-05-10 | Kraftwerk Union AG, 4330 Mülheim | Vormischbrenner mit integriertem diffusionsbrenner |
US4984429A (en) * | 1986-11-25 | 1991-01-15 | General Electric Company | Impingement cooled liner for dry low NOx venturi combustor |
US5117636A (en) * | 1990-02-05 | 1992-06-02 | General Electric Company | Low nox emission in gas turbine system |
US5207064A (en) * | 1990-11-21 | 1993-05-04 | General Electric Company | Staged, mixed combustor assembly having low emissions |
US5257499A (en) * | 1991-09-23 | 1993-11-02 | General Electric Company | Air staged premixed dry low NOx combustor with venturi modulated flow split |
US5638674A (en) * | 1993-07-07 | 1997-06-17 | Mowill; R. Jan | Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission |
US6220034B1 (en) | 1993-07-07 | 2001-04-24 | R. Jan Mowill | Convectively cooled, single stage, fully premixed controllable fuel/air combustor |
US5628182A (en) * | 1993-07-07 | 1997-05-13 | Mowill; R. Jan | Star combustor with dilution ports in can portions |
US5572862A (en) * | 1993-07-07 | 1996-11-12 | Mowill Rolf Jan | Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules |
US5377483A (en) * | 1993-07-07 | 1995-01-03 | Mowill; R. Jan | Process for single stage premixed constant fuel/air ratio combustion |
US5613357A (en) * | 1993-07-07 | 1997-03-25 | Mowill; R. Jan | Star-shaped single stage low emission combustor system |
DE4408136A1 (de) * | 1994-03-10 | 1995-09-14 | Bmw Rolls Royce Gmbh | Verfahren und Vorrichtung zur Kraftstoff-Aufbereitung für eine Gasturbinen-Brennkammer |
DE69506308T2 (de) * | 1994-04-20 | 1999-08-26 | Rolls-Royce Plc | Brennstoffeinspritzdüse für Gasturbinentriebwerke |
DE19507088B4 (de) * | 1995-03-01 | 2005-01-27 | Alstom | Vormischbrenner |
DE19512645A1 (de) * | 1995-04-05 | 1996-10-10 | Bmw Rolls Royce Gmbh | Vorrichtung zur Kraftstoffaufbereitung für eine Brennkammer |
DE19516798A1 (de) * | 1995-05-08 | 1996-11-14 | Abb Management Ag | Vormischbrenner mit axialer oder radialer Luftzuströmung |
DE19527453B4 (de) * | 1995-07-27 | 2009-05-07 | Alstom | Vormischbrenner |
GB2307980B (en) * | 1995-12-06 | 2000-07-05 | Europ Gas Turbines Ltd | A fuel injector arrangement; a method of operating a fuel injector arrangement |
DE19547912A1 (de) * | 1995-12-21 | 1997-06-26 | Abb Research Ltd | Brenner für einen Wärmeerzeuger |
DE19547913A1 (de) * | 1995-12-21 | 1997-06-26 | Abb Research Ltd | Brenner für einen Wärmeerzeuger |
US5924276A (en) * | 1996-07-17 | 1999-07-20 | Mowill; R. Jan | Premixer with dilution air bypass valve assembly |
JP3706443B2 (ja) * | 1996-09-24 | 2005-10-12 | 三菱重工業株式会社 | アニュラ型ガスタービン燃焼器 |
DE19649486A1 (de) * | 1996-11-29 | 1998-06-04 | Abb Research Ltd | Brennkammer |
GB2332509B (en) | 1997-12-19 | 2002-06-19 | Europ Gas Turbines Ltd | Fuel/air mixing arrangement for combustion apparatus |
US6272842B1 (en) * | 1999-02-16 | 2001-08-14 | General Electric Company | Combustor tuning |
US6925809B2 (en) | 1999-02-26 | 2005-08-09 | R. Jan Mowill | Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities |
US6253538B1 (en) | 1999-09-27 | 2001-07-03 | Pratt & Whitney Canada Corp. | Variable premix-lean burn combustor |
US6286300B1 (en) | 2000-01-27 | 2001-09-11 | Honeywell International Inc. | Combustor with fuel preparation chambers |
US6508061B2 (en) * | 2001-04-25 | 2003-01-21 | Pratt & Whitney Canada Corp | Diffuser combustor |
US8590313B2 (en) * | 2008-07-30 | 2013-11-26 | Rolls-Royce Corporation | Precision counter-swirl combustor |
US8281597B2 (en) * | 2008-12-31 | 2012-10-09 | General Electric Company | Cooled flameholder swirl cup |
EP2781838B1 (de) * | 2011-11-16 | 2019-04-24 | Mitsubishi Hitachi Power Systems, Ltd. | Gasturbinenbrennkammer |
EP2959134A4 (de) * | 2013-02-19 | 2016-10-19 | United Technologies Corp | Belüftung eines kraftstoffeinspritzsystems für einen gasturbinenmotor |
US9228747B2 (en) * | 2013-03-12 | 2016-01-05 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
EP2789915A1 (de) * | 2013-04-10 | 2014-10-15 | Alstom Technology Ltd | Verfahren zum Betrieb einer Brennkammer und Brennkammer |
CN105899878B (zh) * | 2013-06-18 | 2018-11-13 | 伍德沃德有限公司 | 燃气涡轮燃烧室组件及发动机及相关联的操作方法 |
US9482433B2 (en) | 2013-11-11 | 2016-11-01 | Woodward, Inc. | Multi-swirler fuel/air mixer with centralized fuel injection |
US9587833B2 (en) | 2014-01-29 | 2017-03-07 | Woodward, Inc. | Combustor with staged, axially offset combustion |
US20150338101A1 (en) * | 2014-05-21 | 2015-11-26 | General Electric Company | Turbomachine combustor including a combustor sleeve baffle |
DE102017120370B4 (de) * | 2017-09-05 | 2019-06-06 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Brennerkopf, Brennersystem und Verfahren zum Betreiben des Brennersystems |
GB202019222D0 (en) | 2020-12-07 | 2021-01-20 | Rolls Royce Plc | Lean burn combustor |
GB202019219D0 (en) * | 2020-12-07 | 2021-01-20 | Rolls Royce Plc | Lean burn combustor |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1790927A (en) * | 1931-02-03 | kreager | ||
US1136849A (en) * | 1912-10-03 | 1915-04-20 | Edwin W Tucker | Fuel-oil-burning apparatus. |
US2531538A (en) * | 1948-05-06 | 1950-11-28 | Cecil W Smith | Air control unit for oil burners |
US3007515A (en) * | 1955-11-14 | 1961-11-07 | John M Furdock | Oil burners |
-
1974
- 1974-08-29 US US501739A patent/US3905192A/en not_active Expired - Lifetime
-
1975
- 1975-08-26 CA CA234,329A patent/CA1028511A/en not_active Expired
- 1975-08-29 JP JP50104875A patent/JPS5185033A/ja active Pending
- 1975-08-29 FR FR7526598A patent/FR2283321A1/fr active Granted
- 1975-08-29 DE DE19752538512 patent/DE2538512A1/de not_active Withdrawn
- 1975-08-29 SE SE7509617A patent/SE7509617L/xx unknown
- 1975-08-29 IT IT26710/75A patent/IT1042151B/it active
- 1975-08-29 GB GB35665/75A patent/GB1489496A/en not_active Expired
- 1975-09-03 IN IN1705/CAL/75A patent/IN142712B/en unknown
Also Published As
Publication number | Publication date |
---|---|
SE7509617L (sv) | 1976-03-01 |
FR2283321B1 (de) | 1980-01-04 |
IT1042151B (it) | 1980-01-30 |
JPS5185033A (de) | 1976-07-26 |
GB1489496A (en) | 1977-10-19 |
FR2283321A1 (fr) | 1976-03-26 |
IN142712B (de) | 1977-08-20 |
DE2538512A1 (de) | 1976-03-11 |
US3905192A (en) | 1975-09-16 |
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