DE60332465D1 - Aftstoffeinspritzdüse - Google Patents
AftstoffeinspritzdüseInfo
- Publication number
- DE60332465D1 DE60332465D1 DE60332465T DE60332465T DE60332465D1 DE 60332465 D1 DE60332465 D1 DE 60332465D1 DE 60332465 T DE60332465 T DE 60332465T DE 60332465 T DE60332465 T DE 60332465T DE 60332465 D1 DE60332465 D1 DE 60332465D1
- Authority
- DE
- Germany
- Prior art keywords
- aftstoffeinspritzdüse
- 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 - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/106—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet
- F23D11/107—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet at least one of both being subjected to a swirling motion
-
- 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
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2211/00—Thermal dilatation prevention or compensation
-
- 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
- F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
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)
- Spray-Type Burners (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/232,397 US6823677B2 (en) | 2002-09-03 | 2002-09-03 | Stress relief feature for aerated gas turbine fuel injector |
PCT/CA2003/001254 WO2004023038A1 (en) | 2002-09-03 | 2003-08-22 | Stress relief feature for aerated gas turbine fuel injector |
Publications (1)
Publication Number | Publication Date |
---|---|
DE60332465D1 true DE60332465D1 (de) | 2010-06-17 |
Family
ID=31976995
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60332465T Expired - Lifetime DE60332465D1 (de) | 2002-09-03 | 2003-08-22 | Aftstoffeinspritzdüse |
Country Status (5)
Country | Link |
---|---|
US (1) | US6823677B2 (de) |
EP (1) | EP1540247B1 (de) |
CA (1) | CA2496908C (de) |
DE (1) | DE60332465D1 (de) |
WO (1) | WO2004023038A1 (de) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6883332B2 (en) * | 1999-05-07 | 2005-04-26 | Parker-Hannifin Corporation | Fuel nozzle for turbine combustion engines having aerodynamic turning vanes |
US7117678B2 (en) * | 2004-04-02 | 2006-10-10 | Pratt & Whitney Canada Corp. | Fuel injector head |
US8348180B2 (en) | 2004-06-09 | 2013-01-08 | Delavan Inc | Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
US7533531B2 (en) * | 2005-04-01 | 2009-05-19 | Pratt & Whitney Canada Corp. | Internal fuel manifold with airblast nozzles |
US7559202B2 (en) * | 2005-11-15 | 2009-07-14 | Pratt & Whitney Canada Corp. | Reduced thermal stress fuel nozzle assembly |
US8015815B2 (en) * | 2007-04-18 | 2011-09-13 | Parker-Hannifin Corporation | Fuel injector nozzles, with labyrinth grooves, for gas turbine engines |
US20090320483A1 (en) * | 2008-06-26 | 2009-12-31 | General Electric Company | Variable Orifice Plug for Turbine Fuel Nozzle |
US20100162714A1 (en) * | 2008-12-31 | 2010-07-01 | Edward Claude Rice | Fuel nozzle with swirler vanes |
US8096757B2 (en) * | 2009-01-02 | 2012-01-17 | General Electric Company | Methods and apparatus for reducing nozzle stress |
EP2236934A1 (de) * | 2009-03-18 | 2010-10-06 | Siemens Aktiengesellschaft | Brenneranordnung |
US8555649B2 (en) * | 2009-09-02 | 2013-10-15 | Pratt & Whitney Canada Corp. | Fuel nozzle swirler assembly |
GB0918099D0 (en) * | 2009-10-16 | 2009-12-02 | Rolls Royce Plc | Fuel injector mounting system |
GB0918169D0 (en) * | 2009-10-19 | 2009-12-02 | Rolls Royce Plc | Fuel injector mounting system |
EP2327933A1 (de) * | 2009-11-30 | 2011-06-01 | Siemens Aktiengesellschaft | Brenneranordnung |
US10317081B2 (en) | 2011-01-26 | 2019-06-11 | United Technologies Corporation | Fuel injector assembly |
US9052113B1 (en) | 2011-06-06 | 2015-06-09 | General Electric Company | Combustor nozzle and method for modifying the combustor nozzle |
US8794544B2 (en) | 2011-06-06 | 2014-08-05 | General Electric Company | Combustor nozzle and method for modifying the combustor nozzle |
US9777637B2 (en) | 2012-03-08 | 2017-10-03 | General Electric Company | Gas turbine fuel flow measurement using inert gas |
US9447974B2 (en) | 2012-09-13 | 2016-09-20 | United Technologies Corporation | Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine |
US9400104B2 (en) | 2012-09-28 | 2016-07-26 | United Technologies Corporation | Flow modifier for combustor fuel nozzle tip |
EP2923150B1 (de) * | 2012-11-21 | 2018-09-05 | General Electric Company | Flüssigbrennstoffkartusche mit anti-verkokungs-funktion |
GB201303428D0 (en) * | 2013-02-27 | 2013-04-10 | Rolls Royce Plc | A vane structure and a method of manufacturing a vane structure |
US20160033130A1 (en) * | 2013-03-15 | 2016-02-04 | United Technologies Corporation | Fuel nozzle for a gas turbine engine |
US9556795B2 (en) * | 2013-09-06 | 2017-01-31 | Delavan Inc | Integrated heat shield |
EP3066321B1 (de) * | 2013-11-04 | 2018-08-29 | United Technologies Corporation | Gekühltes kraftstoffeinspritzsystem für einen gasturbinenmotor und verfahren dazu |
US10557630B1 (en) | 2019-01-15 | 2020-02-11 | Delavan Inc. | Stackable air swirlers |
DE102019103640A1 (de) * | 2019-02-13 | 2020-08-13 | Mitsubishi Hitachi Power Systems Europe Gmbh | Brennstoffdüse mit Dehnungsschlitzen für einen Kohlenstaubbrenner |
US11060460B1 (en) * | 2019-04-01 | 2021-07-13 | Marine Turbine Technologies, LLC | Fuel distribution system for gas turbine engine |
EP3748231B1 (de) * | 2019-06-05 | 2023-08-30 | Siemens Energy Global GmbH & Co. KG | Brenner und brennerspitze |
US11639795B2 (en) | 2021-05-14 | 2023-05-02 | Pratt & Whitney Canada Corp. | Tapered fuel gallery for a fuel nozzle |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2959355A (en) * | 1958-07-25 | 1960-11-08 | Sandberg Serrell Corp | Nozzle |
US3064425A (en) | 1959-10-05 | 1962-11-20 | Gen Motors Corp | Combustion liner |
US3692372A (en) | 1971-06-24 | 1972-09-19 | Gen Electric | Thermally expansible bearing assembly |
US4536932A (en) | 1982-11-22 | 1985-08-27 | United Technologies Corporation | Method for eliminating low cycle fatigue cracking in integrally bladed disks |
US5255508A (en) | 1991-11-01 | 1993-10-26 | United Technologies Corporation | Fuel nozzle assembly and method for making the assembly |
US5222357A (en) * | 1992-01-21 | 1993-06-29 | Westinghouse Electric Corp. | Gas turbine dual fuel nozzle |
US5535585A (en) | 1994-12-13 | 1996-07-16 | Eichhorn; Gunther | Slotted exhaust liner |
JP3710099B2 (ja) * | 1995-03-31 | 2005-10-26 | 株式会社アイ・エイチ・アイ・エアロスペース | ジェッタベータ |
US6082113A (en) * | 1998-05-22 | 2000-07-04 | Pratt & Whitney Canada Corp. | Gas turbine fuel injector |
US6289676B1 (en) * | 1998-06-26 | 2001-09-18 | Pratt & Whitney Canada Corp. | Simplex and duplex injector having primary and secondary annular lud channels and primary and secondary lud nozzles |
US6149075A (en) | 1999-09-07 | 2000-11-21 | General Electric Company | Methods and apparatus for shielding heat from a fuel nozzle stem of fuel nozzle |
-
2002
- 2002-09-03 US US10/232,397 patent/US6823677B2/en not_active Expired - Lifetime
-
2003
- 2003-08-22 WO PCT/CA2003/001254 patent/WO2004023038A1/en not_active Application Discontinuation
- 2003-08-22 DE DE60332465T patent/DE60332465D1/de not_active Expired - Lifetime
- 2003-08-22 CA CA2496908A patent/CA2496908C/en not_active Expired - Lifetime
- 2003-08-22 EP EP03793514A patent/EP1540247B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
CA2496908C (en) | 2011-03-22 |
US6823677B2 (en) | 2004-11-30 |
CA2496908A1 (en) | 2004-03-18 |
EP1540247A1 (de) | 2005-06-15 |
WO2004023038A1 (en) | 2004-03-18 |
EP1540247B1 (de) | 2010-05-05 |
US20040040310A1 (en) | 2004-03-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |