DE502004004752D1 - Offen gekühltes bauteil für eine gasturbine, brennkammer und gasturbine - Google Patents
Offen gekühltes bauteil für eine gasturbine, brennkammer und gasturbineInfo
- Publication number
- DE502004004752D1 DE502004004752D1 DE502004004752T DE502004004752T DE502004004752D1 DE 502004004752 D1 DE502004004752 D1 DE 502004004752D1 DE 502004004752 T DE502004004752 T DE 502004004752T DE 502004004752 T DE502004004752 T DE 502004004752T DE 502004004752 D1 DE502004004752 D1 DE 502004004752D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- combustion chamber
- cooled component
- open cooled
- open
- 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.)
- Active
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
- F23R3/28—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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/186—Film cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M5/00—Casings; Linings; Walls
- F23M5/08—Cooling thereof; Tube walls
- F23M5/085—Cooling thereof; Tube walls using air or other gas as the cooling medium
-
- 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
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP03015216 | 2003-07-04 | ||
PCT/EP2004/006491 WO2005003517A1 (de) | 2003-07-04 | 2004-06-16 | Offen gekühltes bauteil für eine gasturbine, brennkammer und gasturbine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE502004004752D1 true DE502004004752D1 (de) | 2007-10-04 |
Family
ID=33560756
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE502004004752T Active DE502004004752D1 (de) | 2003-07-04 | 2004-06-16 | Offen gekühltes bauteil für eine gasturbine, brennkammer und gasturbine |
Country Status (7)
Country | Link |
---|---|
US (2) | US7658076B2 (de) |
EP (1) | EP1651841B1 (de) |
CN (1) | CN100353032C (de) |
DE (1) | DE502004004752D1 (de) |
ES (1) | ES2288687T3 (de) |
PL (1) | PL1651841T3 (de) |
WO (1) | WO2005003517A1 (de) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1847696A1 (de) * | 2006-04-21 | 2007-10-24 | Siemens Aktiengesellschaft | Bauteil für eine gestufte Verbrennung in einer Gasturbine und entsprechende Gasturbine. |
EP1847684A1 (de) * | 2006-04-21 | 2007-10-24 | Siemens Aktiengesellschaft | Turbinenschaufel |
US20080134685A1 (en) * | 2006-12-07 | 2008-06-12 | Ronald Scott Bunker | Gas turbine guide vanes with tandem airfoils and fuel injection and method of use |
US8291705B2 (en) * | 2008-08-13 | 2012-10-23 | General Electric Company | Ultra low injection angle fuel holes in a combustor fuel nozzle |
EP2411736B1 (de) * | 2009-02-26 | 2019-06-05 | 8 Rivers Capital, LLC | Vorrichtung und verfahren zur verbrennung eines brennstoffs bei hohem druck und hoher temperatur und zugehörige(s) system und vorrichtung |
US8986002B2 (en) | 2009-02-26 | 2015-03-24 | 8 Rivers Capital, Llc | Apparatus for combusting a fuel at high pressure and high temperature, and associated system |
US9068743B2 (en) * | 2009-02-26 | 2015-06-30 | 8 Rivers Capital, LLC & Palmer Labs, LLC | Apparatus for combusting a fuel at high pressure and high temperature, and associated system |
US8397516B2 (en) * | 2009-10-01 | 2013-03-19 | General Electric Company | Apparatus and method for removing heat from a gas turbine |
US8959886B2 (en) * | 2010-07-08 | 2015-02-24 | Siemens Energy, Inc. | Mesh cooled conduit for conveying combustion gases |
US8894363B2 (en) | 2011-02-09 | 2014-11-25 | Siemens Energy, Inc. | Cooling module design and method for cooling components of a gas turbine system |
US8640974B2 (en) | 2010-10-25 | 2014-02-04 | General Electric Company | System and method for cooling a nozzle |
US9249977B2 (en) * | 2011-11-22 | 2016-02-02 | Mitsubishi Hitachi Power Systems, Ltd. | Combustor with acoustic liner |
US9284231B2 (en) | 2011-12-16 | 2016-03-15 | General Electric Company | Hydrocarbon film protected refractory carbide components and use |
DE102012205055B4 (de) * | 2012-03-29 | 2020-08-06 | Detlef Haje | Gasturbinenbauteil für Hochtemperaturanwendungen, sowie Verfahren zum Betreiben und Herstellen eines solchen Gasturbinenbauteils |
US9174309B2 (en) | 2012-07-24 | 2015-11-03 | General Electric Company | Turbine component and a process of fabricating a turbine component |
US9709274B2 (en) | 2013-03-15 | 2017-07-18 | Rolls-Royce Plc | Auxetic structure with stress-relief features |
EP2846096A1 (de) * | 2013-09-09 | 2015-03-11 | Siemens Aktiengesellschaft | Rohrbrennkammer mit einem Flammrohr-Endbereich und Gasturbine |
DE102015111843A1 (de) * | 2015-07-21 | 2017-01-26 | Rolls-Royce Deutschland Ltd & Co Kg | Turbine mit gekühlten Turbinenleitschaufeln |
US20170176012A1 (en) * | 2015-12-22 | 2017-06-22 | General Electric Company | Fuel injectors and staged fuel injection systems in gas turbines |
MX2019010632A (es) | 2017-03-07 | 2019-10-15 | 8 Rivers Capital Llc | Sistema y metodo para la operacion de una camara de combustion de combustible flexible para turbina de gas. |
CA3055403A1 (en) | 2017-03-07 | 2018-09-13 | 8 Rivers Capital, Llc | System and method for combustion of solid fuels and derivatives thereof |
WO2020021456A1 (en) | 2018-07-23 | 2020-01-30 | 8 Rivers Capital, Llc | System and method for power generation with flameless combustion |
CN113202566B (zh) * | 2021-04-19 | 2022-12-02 | 中国航发湖南动力机械研究所 | 涡轮导向叶片及燃气涡轮发动机 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2647368A (en) * | 1949-05-09 | 1953-08-04 | Hermann Oestrich | Method and apparatus for internally cooling gas turbine blades with air, fuel, and water |
US2981066A (en) * | 1956-04-12 | 1961-04-25 | Elmer G Johnson | Turbo machine |
US3037351A (en) * | 1956-05-14 | 1962-06-05 | Paul O Tobeler | Combustion turbine |
US4347037A (en) * | 1979-02-05 | 1982-08-31 | The Garrett Corporation | Laminated airfoil and method for turbomachinery |
GB2049152B (en) * | 1979-05-01 | 1983-05-18 | Rolls Royce | Perforate laminated material |
US4302940A (en) * | 1979-06-13 | 1981-12-01 | General Motors Corporation | Patterned porous laminated material |
US4928481A (en) * | 1988-07-13 | 1990-05-29 | Prutech Ii | Staged low NOx premix gas turbine combustor |
US5405242A (en) * | 1990-07-09 | 1995-04-11 | United Technologies Corporation | Cooled vane |
US5125793A (en) | 1991-07-08 | 1992-06-30 | The United States Of America As Represented By The Secretary Of The Air Force | Turbine blade cooling with endothermic fuel |
US5486093A (en) * | 1993-09-08 | 1996-01-23 | United Technologies Corporation | Leading edge cooling of turbine airfoils |
GB2310896A (en) | 1996-03-05 | 1997-09-10 | Rolls Royce Plc | Air cooled wall |
US6047550A (en) | 1996-05-02 | 2000-04-11 | General Electric Co. | Premixing dry low NOx emissions combustor with lean direct injection of gas fuel |
DE19737845C2 (de) | 1997-08-29 | 1999-12-02 | Siemens Ag | Verfahren zum Herstellen einer Gasturbinenschaufel, sowie nach dem Verfahren hergestellte Gasturbinenschaufel |
US20030024234A1 (en) * | 2001-08-02 | 2003-02-06 | Siemens Westinghouse Power Corporation | Secondary combustor for low NOx gas combustion turbine |
US7217088B2 (en) * | 2005-02-02 | 2007-05-15 | Siemens Power Generation, Inc. | Cooling fluid preheating system for an airfoil in a turbine engine |
-
2004
- 2004-06-16 PL PL04739955T patent/PL1651841T3/pl unknown
- 2004-06-16 US US10/561,641 patent/US7658076B2/en not_active Expired - Fee Related
- 2004-06-16 DE DE502004004752T patent/DE502004004752D1/de active Active
- 2004-06-16 CN CNB2004800166533A patent/CN100353032C/zh not_active Expired - Fee Related
- 2004-06-16 WO PCT/EP2004/006491 patent/WO2005003517A1/de active IP Right Grant
- 2004-06-16 ES ES04739955T patent/ES2288687T3/es active Active
- 2004-06-16 EP EP04739955A patent/EP1651841B1/de not_active Not-in-force
-
2009
- 2009-12-07 US US12/631,940 patent/US8347632B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US8347632B2 (en) | 2013-01-08 |
EP1651841B1 (de) | 2007-08-22 |
ES2288687T3 (es) | 2008-01-16 |
CN1806094A (zh) | 2006-07-19 |
US7658076B2 (en) | 2010-02-09 |
CN100353032C (zh) | 2007-12-05 |
EP1651841A1 (de) | 2006-05-03 |
PL1651841T3 (pl) | 2008-01-31 |
US20100083665A1 (en) | 2010-04-08 |
US20070101722A1 (en) | 2007-05-10 |
WO2005003517A1 (de) | 2005-01-13 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE502004004752D1 (de) | Offen gekühltes bauteil für eine gasturbine, brennkammer und gasturbine | |
DE60227769D1 (de) | Brennkammer für Gasturbine | |
DE60224141D1 (de) | Gasturbine und Brennkammer dafür | |
DE112005001800T5 (de) | Gehäuse und Gasturbine | |
DE602005009084D1 (de) | Bläseranordnung für eine Gasturbine | |
DE60203959D1 (de) | Luftgekühltes Abgasgehäuse für eine Gasturbine | |
DE60229019D1 (de) | Zerlegbarer Aufsatz für eine Gasturbinenbrennkammer | |
DE502004011910D1 (de) | Stationäre gasturbine | |
DE60112030D1 (de) | Kühlstruktur für eine Gasturbine | |
DE60323417D1 (de) | Gasturbinenverbrennungskammer | |
DE60105531D1 (de) | Gasturbinenbrennkammer, Gasturbine und Düsentriebwerk | |
DE60012289D1 (de) | Brennkammer für eine Gasturbine | |
GB0612608D0 (en) | Gas turbine engine and method of operating same | |
DE602005007391D1 (de) | Gasturbinentriebwerk | |
DE60236991D1 (de) | Befestigungsvorrichtung für Gasturbinenbrennkammer | |
ATE310896T1 (de) | Übergangstück für eine nicht-ringförmige gasturbinenbrennkammer | |
DE602005001682D1 (de) | Helmholtzresonator für eine Brennkammer eines Gasturbinentriebwerks | |
DE60313392D1 (de) | Gasturbine | |
EP1706620A4 (de) | Turbomotorarchitektur | |
DE602005001528D1 (de) | Gasturbinentriebwerk | |
GB0304320D0 (en) | Gas turbine engines | |
DE102004003354A8 (de) | Turbinen-Laufschaufel und Gasturbine | |
DE50309686D1 (de) | Gasturbine | |
DE60320344D1 (de) | Brennkammer für eine Gasturbine und Verfahren zur Kontrolle der Verbrennung | |
DE502004004513D1 (de) | Rotor für eine gasturbine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |