DE69633535D1 - Brennkammer und Verfahren zum Betrieb einer mit gasförmigen oder flüssigem Brennstoff betriebenen Gasturbine - Google Patents
Brennkammer und Verfahren zum Betrieb einer mit gasförmigen oder flüssigem Brennstoff betriebenen GasturbineInfo
- Publication number
- DE69633535D1 DE69633535D1 DE69633535T DE69633535T DE69633535D1 DE 69633535 D1 DE69633535 D1 DE 69633535D1 DE 69633535 T DE69633535 T DE 69633535T DE 69633535 T DE69633535 T DE 69633535T DE 69633535 D1 DE69633535 D1 DE 69633535D1
- Authority
- DE
- Germany
- Prior art keywords
- gaseous
- operating
- combustion chamber
- gas turbine
- liquid fuel
- 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 - Fee Related
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
- F23R3/002—Wall structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/20—Heat transfer, e.g. cooling
- F05B2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
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 (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9505067 | 1995-03-14 | ||
GBGB9505067.0A GB9505067D0 (en) | 1995-03-14 | 1995-03-14 | Combustor and operating method for gas or liquid-fuelled turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69633535D1 true DE69633535D1 (de) | 2004-11-11 |
DE69633535T2 DE69633535T2 (de) | 2005-10-13 |
Family
ID=10771134
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69633535T Expired - Fee Related DE69633535T2 (de) | 1995-03-14 | 1996-02-22 | Brennkammer und Verfahren zum Betrieb einer mit gasförmigen oder flüssigem Brennstoff betriebenen Gasturbine |
Country Status (5)
Country | Link |
---|---|
US (1) | US5784876A (de) |
EP (1) | EP0732546B1 (de) |
JP (1) | JP3833297B2 (de) |
DE (1) | DE69633535T2 (de) |
GB (1) | GB9505067D0 (de) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6240731B1 (en) * | 1997-12-31 | 2001-06-05 | United Technologies Corporation | Low NOx combustor for gas turbine engine |
US6098397A (en) * | 1998-06-08 | 2000-08-08 | Caterpillar Inc. | Combustor for a low-emissions gas turbine engine |
US6349467B1 (en) * | 1999-09-01 | 2002-02-26 | General Electric Company | Process for manufacturing deflector plate for gas turbin engine combustors |
US6484505B1 (en) * | 2000-02-25 | 2002-11-26 | General Electric Company | Combustor liner cooling thimbles and related method |
DE10064264B4 (de) * | 2000-12-22 | 2017-03-23 | General Electric Technology Gmbh | Anordnung zur Kühlung eines Bauteils |
JP3985027B2 (ja) * | 2001-03-01 | 2007-10-03 | 独立行政法人 宇宙航空研究開発機構 | 燃焼試験装置 |
US6543231B2 (en) * | 2001-07-13 | 2003-04-08 | Pratt & Whitney Canada Corp | Cyclone combustor |
US6609362B2 (en) | 2001-07-13 | 2003-08-26 | Pratt & Whitney Canada Corp. | Apparatus for adjusting combustor cycle |
JP2003074856A (ja) * | 2001-08-28 | 2003-03-12 | Honda Motor Co Ltd | ガスタービン・エンジンの燃焼器 |
GB2390150A (en) * | 2002-06-26 | 2003-12-31 | Alstom | Reheat combustion system for a gas turbine including an accoustic screen |
US7010921B2 (en) * | 2004-06-01 | 2006-03-14 | General Electric Company | Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
US7574865B2 (en) * | 2004-11-18 | 2009-08-18 | Siemens Energy, Inc. | Combustor flow sleeve with optimized cooling and airflow distribution |
US7360364B2 (en) * | 2004-12-17 | 2008-04-22 | General Electric Company | Method and apparatus for assembling gas turbine engine combustors |
DE102005059184B3 (de) * | 2005-12-02 | 2007-09-06 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Vorrichtung und Verfahren zur Dämpfung thermoakustischer Resonanzen in Brennkammern |
DE102006042124B4 (de) * | 2006-09-07 | 2010-04-22 | Man Turbo Ag | Gasturbinenbrennkammer |
MY148889A (en) * | 2007-02-06 | 2013-06-14 | Basf Se | Method for providing a as gas flow comprising oxygen for the endothermic reaction of a starting flow comprising one or more hydrocarbons |
US8051663B2 (en) | 2007-11-09 | 2011-11-08 | United Technologies Corp. | Gas turbine engine systems involving cooling of combustion section liners |
US20090165435A1 (en) | 2008-01-02 | 2009-07-02 | Michal Koranek | Dual fuel can combustor with automatic liquid fuel purge |
US8096133B2 (en) * | 2008-05-13 | 2012-01-17 | General Electric Company | Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface |
US8109099B2 (en) * | 2008-07-09 | 2012-02-07 | United Technologies Corporation | Flow sleeve with tabbed direct combustion liner cooling air |
US8291711B2 (en) | 2008-07-25 | 2012-10-23 | United Technologies Corporation | Flow sleeve impingement cooling baffles |
US8677759B2 (en) * | 2009-01-06 | 2014-03-25 | General Electric Company | Ring cooling for a combustion liner and related method |
DE102009035550A1 (de) | 2009-07-31 | 2011-02-03 | Man Diesel & Turbo Se | Gasturbinenbrennkammer |
EP2299178B1 (de) * | 2009-09-17 | 2015-11-04 | Alstom Technology Ltd | Verfahren und Gasturbinenverbrennungssystem zum sicheren Mischen von H2-reichen Brennstoffen mit Luft |
US9423132B2 (en) * | 2010-11-09 | 2016-08-23 | Opra Technologies B.V. | Ultra low emissions gas turbine combustor |
US8844260B2 (en) * | 2010-11-09 | 2014-09-30 | Opra Technologies B.V. | Low calorific fuel combustor for gas turbine |
US9989260B2 (en) * | 2015-12-22 | 2018-06-05 | General Electric Company | Staged fuel and air injection in combustion systems of gas turbines |
EP3832209A1 (de) * | 2017-07-25 | 2021-06-09 | GE Avio S.r.l. | Umlenkbrennkammer |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4205524A (en) * | 1974-03-29 | 1980-06-03 | Phillips Petroleum Company | Methods of operating combustors |
GB1537109A (en) * | 1975-10-23 | 1978-12-29 | Gen Electric | Gas turbine combustion system |
US4008568A (en) * | 1976-03-01 | 1977-02-22 | General Motors Corporation | Combustor support |
GB2125950B (en) * | 1982-08-16 | 1986-09-24 | Gen Electric | Gas turbine combustor |
US4567730A (en) * | 1983-10-03 | 1986-02-04 | General Electric Company | Shielded combustor |
GB2176274B (en) * | 1985-06-07 | 1989-02-01 | Ruston Gas Turbines Ltd | Combustor for gas turbine engine |
US5363654A (en) * | 1993-05-10 | 1994-11-15 | General Electric Company | Recuperative impingement cooling of jet engine components |
-
1995
- 1995-03-14 GB GBGB9505067.0A patent/GB9505067D0/en active Pending
-
1996
- 1996-02-21 US US08/604,675 patent/US5784876A/en not_active Expired - Fee Related
- 1996-02-22 DE DE69633535T patent/DE69633535T2/de not_active Expired - Fee Related
- 1996-02-22 EP EP96301212A patent/EP0732546B1/de not_active Expired - Lifetime
- 1996-03-05 JP JP07513396A patent/JP3833297B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0732546A1 (de) | 1996-09-18 |
JPH08246900A (ja) | 1996-09-24 |
GB9505067D0 (en) | 1995-05-03 |
EP0732546B1 (de) | 2004-10-06 |
DE69633535T2 (de) | 2005-10-13 |
US5784876A (en) | 1998-07-28 |
JP3833297B2 (ja) | 2006-10-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69633535D1 (de) | Brennkammer und Verfahren zum Betrieb einer mit gasförmigen oder flüssigem Brennstoff betriebenen Gasturbine | |
DE69523082D1 (de) | Brennstoffdüse einer Turbine mit doppelter Möglichkeit zur Diffusions- und Vormischverbrennung und Verfahren zum Betrieb | |
DE59305562D1 (de) | Verfahren zum Betrieb einer Brennkammer einer Gasturbine | |
DE59810344D1 (de) | Verfahren zum Betrieb einer Gasturbinenbrennkammer mit gasförmigem Brennstoff | |
DE59402785D1 (de) | Brenner zum Betrieb einer Brennkraftmaschine, einer Brennkammer einer Gasturbogruppe oder Feuerungsanlage | |
DE59407984D1 (de) | Vormischbrenner zum Betrieb einer Brennkraftmaschine, einer Brennkammer einer Gasturbogruppe oder Feuerungsanlage | |
SG53096A1 (en) | Liquid pilot fuel injection method and apparatus for a gas turbine engine dual fuel injector | |
DE69616881T2 (de) | Verfahren und Vorrichtung zur Verringerung der NOx-Emissionen eines Gasbrenners | |
DE69302585D1 (de) | Brennstoffverteilerventil für eine gasturbine | |
DE69610240D1 (de) | Einrichtung zum Vorwärmen von Brennstoff für eine Gasturbine | |
NO934890L (no) | Trimmesystem for brennstoff til et forbrenningssystem i en gassturbin med flere brennkamre | |
DE59610114D1 (de) | Verfahren zum Betrieb einer mit einem Abhitzedampferzeuger und einem Dampfverbraucher kombinierten Gasturbogruppe | |
DE69632111D1 (de) | Vormischbrenner für eine Gasturbinenbrennkammer mit niedriger Schadstoffemission | |
DE69506308D1 (de) | Brennstoffeinspritzdüse für Gasturbinentriebwerke | |
DE69421896T2 (de) | Umleitungsventil für die Brennkammer einer Gasturbine | |
DE59504264D1 (de) | Brennkammer für eine gasturbine | |
DE69414733D1 (de) | Verfahren zum Betrieb eines Mantelstromtriebwerkes mit schwenkbaren Leitschaufeln | |
DE59710441D1 (de) | Brenner und Verfahren zum Betrieb einer Brennkammer mit einem flüssigen und/oder gasförmigen Brennstoff | |
DE69610274T2 (de) | Brennstoffregeleinrichtung für Gasturbine | |
DE69922559D1 (de) | Verfahren zum Betreiben einer Gasturbinenbrennkammer für flüssigen Kraftstoff | |
DE59609859D1 (de) | Verfahren zum betrieb einer gasturbogruppe mit niederkalorischem brennstoff | |
DE69127555D1 (de) | Emissionsarme verbrennungsdüse zum gebrauch in einem gasturbinentriebwerk | |
DE59811336D1 (de) | Verfahren zum Betrieb einer Gasturbinenbrennkammer mit flüssigem Brennstoff | |
DE59610422D1 (de) | Verfahren und Vorrichtung zur Schnellumschaltung vom Vormischbetrieb in den Diffusionsbetrieb in einer Brennkammer einer mit Brenngas betriebenen Gasturbine | |
DE69609785D1 (de) | Kraftstoffeinspritzverfahren für einen Gasmotor und dazugehöriger Gasmotor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: SIEMENS AG, 80333 MUENCHEN, DE |
|
8339 | Ceased/non-payment of the annual fee |